Sikorsky

 

Developed in 1954 as a multirole helicopter.  Known as H-34A Choctaw by the U.S. Army, HUS-1 in the U.S. Marines, and HSS-1 in the U.S. Navy as an ASW helicopter.

 

 

Image coming soon!

Overview
Parent type
Variant
Design authority Sikorsky Aircraft Corp.
Primary manufacturer Sikorsky Aircraft Corp.
Key Characteristics
Operational status No longer flying
Max gross weight (ground) 6,350 n/a 6,350 n/a
Crew 0
Seating arrangement Side-by-side
Configuration
VTOL type Helicopter
Compound type None
Lift configuration Single main rotor
Control device type Tail rotor
Features
Number of engines 1
Number of propulsors 0
Number of lift devices 1
Number of control devices 1

Sikorsky

 

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Sikorsky

 

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Sikorsky

 

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Sikorsky

 

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Sikorsky

 

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Sikorsky

 

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Sikorsky

 

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A Comparative Study of Tail Rotor Noise Mechanisms
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A Comparison of Three Coaxial Aerodynamic Prediction Methods Including Validation With Model Test Data
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A Comparison: Weak Versus Strong Modular Coupling for Trimmed Aeroelastic Rotor Simulations
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A Composite Beam Finite Element Model with p-version Assumed Warping Displacement
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A Composite Pylon Support Structure for the JetRanger Helicopter
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A Composite Rotor Blade Structural Design Environment for Aeromechanical Assessments in Conceptual and Preliminary Design
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A Comprehensive Approach to On-Condition Evaluation of Rotorcraft Structural Integrity
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A Comprehensive Diagnostic System for the T800-APW-800 Engine
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A Comprehensive Hover Test of the Airloads and Airflow of an Extensively Instrumented Model Helicopter Rotor
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A Comprehensive Pilot Model for Voluntary/Involuntary Action in Rotorcraft-Pilot Coupling
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A Comprehensive Plan For Helicopter Drag Reduction
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A Comprehensive Study of Active Microflaps for Vibration Reduction in Rotorcraft
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A Computational Analysis of Parallel Blade-Vortex Interactions using Vorticity Embedding
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A Computational Approach for Model Update of an LS-DYNA Energy Absorbing Cell
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A Computational Framework for Helicopter Fuselage Drag Reduction Using Vortex Generators
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A Computational Method for the Determination of Structural Reliability of Helicopter Dynamic Components
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A Computational Method for the Determination of Structural Reliability of Helicopter Dynamic Components
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A Computational Study of BVI Noise Reduction Using Active Twist Control
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A Computational Study of Helicopter Rotor Wakes and Noise Generated During Transient Maneuvers
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A Computational Study of Trailing-Edge Flap Aerodynamics and Acoustics
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A Computer Program For The Preliminary Design And Assessment Of Future VTOL Configurations
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A Conceptual Optimization Study of a Rotor Blade Internal Structural Arrangement
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A Consistent Crashworthiness Design Criteria Approach for Rotary Wing Aircraft
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A Contemporary Survey of the Structural Performance Standards for Rotary Wing Aircraft Crashworthy Passenger Seating
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A Continuous Ramp Methodology for Vibration in Highly Accelerated Life Testing
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A Control Architecture For Fast And Precise Autonomous Landing Of A VTOL UAV Onto An Oscillating Platform
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A Control Theory Approach to Machinery Health Prognostics
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A Conversation on Systems Engineering Attributes
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A Correlation Study of Rotor Inflow In Forward Flight
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A Correlative Study On Aeroelastic Stability Improvement For Composite Hingeless Hub System By Comparing Analysis And Experimental Results
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A Cost Effective System Safety Approach for Integrating Routine Unmanned Aircraft Systems into the National Airspace System
Dr. Daniel P. Schrage, Georgia Tech

 

A Coupled Rotor/Wing Optimization Procedure for High Speed Tilt-Rotor Aircraft
Thomas R. McCarthy, Aditi Chattopadhyay, and Sen Shang, Arizona State University

 

A Coupled Vortex Particle/CFD Methodology for Studying Coaxial Rotor Configurations
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A Coupled Vortex Particle/CFD Methodology for Studying Coaxial Rotor Configurations
Nischint Rajmohan, Jinggen Zhao, and Chengjian He, Advanced Rotorcraft Technology, Inc.

 

A Coupling Procedure Between A Rotor Dynamics Code And A 3D Unsteady Full Potential Code
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A Crew Workload Evaluation Methodology
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A Critical Examination Of The Flap-Lag Dynamics Of Helicopter Rotor Blades In Hover And In Forward Flight
K. R. V. Kaza; R. G. Kvaternik

 

A Critical Examination of the Methods to Improve the Off-Axis Response Prediction of Helicopters
Jeffrey D. Keller, Continuum Dynamics, Inc.; H.C. Curtiss, Jr., Princeton University

 

A Critical Re-Examination of the Franklin Institute Rotating Wing Aircraft Meeting of October 28 - 29, 1938: Facts and Myths Surrounding the Foundations of Autogiro/Convertiplane/Helicopter Development in America and Europe
B.H. Charnov, Hofstra University

 

A Culture of Innovation
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A Damage Tolerance and Fatigue Evaluation Approach for Composite Rotorcraft Airframe Structures
Alexander Engleder, AIRBUS Helicopters Deutschland

 

A Damage Tolerance/Life Processor For Structural Integrity And Force Management
Preston R. Bates, Georgia Tech Research Institute

 

A Data Mining Based Approach for Gear Fault Diagnostics Using Vibration Sensors
Ruoyu Li, SKF Remote Diagnostic Center; David He, The University of Illinois at Chicago and Praneet Menon, Goodrich SIS

 

A DAVBA Approach for Complex VTOL Aircraft Development
Daniel Schrage, Georgia Tech; Alex Van der Velden, Dassault Systemes

 

A Decomposition Based Optimization Procedure for High Speed Prop-Rotors using Composite Tailoring and Simulated Annealing
Aditi Chattopadhyay, Thomas R. McCarthy, Charles E. Seeley, Arizona State University

 

A Design Handbook for Helicopter Transparent Enclosures
B.F. Kay & J.H. McGarvey

 

A Design Methodology for a Compliant Matrix Composite Bearingless Main Rotor
C.J. Saddler and D.L. Hawkings, Westland Helicopters Ltd.

 

A Design System for Erosion Tolerant Helicopter Engines
B.V.R. Vittal, General Motors Corporation

 

A Design-Support Team Views Forty Years of Commercial Helicopter Value
G.M. Powell and F.J. Wagner, Bell Helicopter Textron, Inc

 

A Detailed Experimental Analysis of Dynamic Stall on an Unsteady Two-Dimensional Airfoil
J. M. Martin, R. W. Empey, and W. J. McCroskey, F. X. Caradonna, USAAMR&DL, Moffett Field, Calif.

 

A Development Program Comparison: CH-47 and the V-22
Eric G. Streich, Boeing Rotorcraft

 

A Direct Adaptive Neural Command Controller Design for an Unstable Helicopter
Kumar, M. Vijaya; Suresh, S.; Omkar, S.N.; Ganguli, Ranjan; Sampath, Prasad

 

A Direct Drive Fly-By-Wire System
Gavin D. Jenney, Dynamic Controls, Inc.

 

A Discrete Crack Network Based Damage Assessment for Bolted Composite Structures
Jim Lua and Neethi Simon and Eugene Fang, Global Engineering and Materials, Inc.; Anisur Rahman and Nam Phan, Naval Air Warefare Center (PAX)

 

A Discussion of CAA Policies, Flight Test Procedures and Civil Air Regulations for Helicopters
Mr. G. DeVore, C.A.A.

 

A Discussion of the Problems in the Selection and Development of Military Helicopter Pilots
William H. Coffee

 

A Discussion of U. S. Army Aircraft Armament Program
Major Donald J. Haid, Chief, U. S. Army Aviation Human Research Unit

 

A Display & Control Concept for Helicopter Flight in Adverse Weather Conditions
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A Dual Compact Model for Rotor Noise Prediction
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A Dual Compact Model for Rotor Noise Prediction
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A Dual-Fan VTOL Aircraft Using Opposed Lateral Tilting for Pitch Control
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A Dual-Stiffness-Energy Sensor for Crack Detection in Spur Gears
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A Dynamic Dual Stiffness Sensor in Helicopter Health and Usage Monitoring
Celestine Wakha, Darryll J. Pines, University of Maryland

 

A Dynamic View for Exercising Functions for Integrated Product and Process Development
Daniel Schrage, Georgia Tech

 

A Dynamics Approach to Helicopter Transmission Noise Reduction and Improved Reliability
R. M. Hartman, Boeing Vertol

 

A Family Of Advanced Turboshaft Engines
W.L. Rodenbaugh

 

A Far Field Boundary and Initial Condition for the Simulation of Hovering Rotors based on Turbulent Jets
Stephen Repsher and Philippe Spalart, The Boeing Company

 

A Fast Adaptive Resolution Method for Efficient Free Wake Calculations
Wayne O. Miller, National Research Council

 

A Fast Kirchhoff Integration Technique for Rotor Noise Directivity Predictions
G. Rahier and J. Zibi, Office National d'Études et de Recherches Aérospatiales

 

A Fault-Tolerant Architecture for Unmanned Rotorcraft
Graham R. Drozeski, Bhaskar Saha, and George Vachtsevanos, Georgia Institute of Technology

 

A Fault-Tolerant Architecture with Reconfigurable Path Planning Applied to an Unmanned Aerial Vehicle
Drozeski, Graham R.; Vachtsevanos, George

 

A Feasibility Study of Using Smart Materials for Rotor Control
Friedrich K. Straub, McDonnell Douglas Helicopter Co.

 

A Finite Element Method to Predict Internal Noise Levels at Discrete Frequencies for a Partially Composite Helicopter Fuselage
F. Chabas, J.M. David, A. Desanti, N. Meidinger, and C. Soize, ONERA, and M. Dussac, P. Martin and H.J. Marze, Aerospatiale

 

A Finite State Inflow Model for Simulation of Helicopter Hovering in Ground Effect
Hong Xin, Georgia Institute of Technology; J.V.R. Prasad, Georgia Institute of Technology; D. A. Peters, Washington University; T. Nagashima, National Defense Academy, N. Iboshi; National Defense Academy

 

A Finite-Volume Euler Solver for Computing Rotary-Wing Aerodynamics on Unstructured Meshes
R.C. Strawn, U.S. Army Aeroflightdynamics Directorate, and T.J. Barth, NASA Ames Research Center

 

A Flight Director/FLIR Helicopter Night Landing System
P.G. Cooper

 

A Flight Dynamics Investigation of Compound Helicopter Configurations
Kevin Ferguson and Douglas Thomson, University of Glasgow

 

A Flight Evaluation of Advanced Control Modes for Manual Recovery of a STOVL Aircraft
Glenn D’Mello, Sqn Ldr Justin Paines RAF, Lt Cdr Ivan Finn RN, Defence Evaluation and Research Agency

 

A Flight Investigation of Control, Display and Guidance Requirements for Decelerating Descending VTOL Instrument Transitions Using the X-22A Variable-Stability Aircraft
J. V. Lebacqz and E. W. Aiken, Calspan Corp.

 

A Flight Investigation of Static Stability, Control Augmentation, and Flight Director Influences on Helicopter IFR Handling Qualities
J. Lebacqz & J. Weber, NASA Ames Research Center, & L. Corliss, U.S. Army Aeromechanics Laboratory

 

A Framework for Cost-Benefit Analysis of Tiltrotor Aircraft
Robert Scott and Daniel Schrage, Georgia Institute of Technology

 

A Framework for Modeling Wind-Farm Wake Turbulence from a Database for Simulation and Analysis
Gopal Gaonkar and Kyle Schau, Florida Atlantic University

 

A Framework for Modeling Wind-Farm Wake Turbulence from a Database for Simulation and Analysis
Gopal Gaonkar and Kyle Schau, Florida Atlantic University

 

A Framework for Modeling Wind-Farm Wake Turbulence from a Database for Simulation and Analysis
Kyle Schau, Gopal Gaonkar, Florida Atlantic University

 

A Free Wake/Ground Vortex Model For Rotors at Low Speed In-Ground-Effect Flight
C. S. Lee and C. J. He, Advanced Rotorcraft Technology, Inc.

 

A Frequency Response Approach to Flying Qualities Criteria and Flight Control System Design
N. Albion and W. R. Larson, Boeing Vertol Co.

 

A Full Mission Simulation Data System
J.A. Edwards, Sikorsky Aircraft

 

A Full Potential Rotor Analysis with Wake Influence Using an Inner-Outer Domain Technique
T.A. Egolf and S.P. Sparks, United Technologies Research Center

 

A Full Scale Airframe High Cycle Fatigue Test Methodology and its Application to the SH-2G Helicopter
P.E. Keary, T. Vothanh, and C.A. Tomashofski, Kaman Aerospace Corp.

 

A Full-Scale Particle Image Velocimetry Investigation of "Young" Rotor Blade Tip Vortices
Kindler, Kolja; Mulleners, Karen; Raffel, M.; Richard, H.

 

A Full-Scale Test of the McDonnell Douglas Advanced Bearingless Rotor in the NASA Ames 40 x 80 Foot Wind Tunnel
Michael McNulty, McDonnell Douglas Helicopter Co.; Stephen Jacklin & Benton Lau, NASA Ames Research Center

 

A Fully Nonlinear Version of the Pitt-Peter Dynamic Inflow Model in Axial Flow
JunSoo Hong, Washington University in Saint Louis

 

A General Approach to Vorticity Confinement Development for High-Order Flow Solvers
Brentner, Kenneth; Hennes, Christopher

 

A General Free Wake Geometry Calculation for Wings and Rotors
Ted Trept, David Sigl, Dan Robertson, Bell Helicopter Textron, Inc.

 

A Generalised Model for Airfoil Unsteady Aerodynamic Behaviour and Dynamic Stall Using the Indicial Method
J.G. Leishman and T.S. Beddoes, Westland Helicopter Ltd

 

A Generalized Dynamic Balancing Procedure for the AH-64 Tail Rotor
Kunz, Donald; Newkirk, Mark

 

A Generalized Dynamic Wake Model with Wake Distortion Effects
Krishnamohan R. Krothapalli, Georgia Institute of Technology; J.V.R. Prasad, Georgia Institute of Technology; David A. Peters, Washington University

 

A Generalized Model for Transiotional Blade Tip Vortices
Leishman, J. Gordon; Ramasamy, Manikandan

 

A Generalized Sling Load Model for the V-22 FFS
Lagace, Glenn

 

A Generic Rotorcraft Simulation Using Matlab/Simulink
Fertman, Alexander; Friedman, Chen; Rand, Omri

 

A Glance At Soviet Helicopter Design Philosophy
W.Z. Stepniewski, Boeing Vertol Company

 

A GPU Accelerated Navier-Stokes Solver for Rotorcraft Applications
Sebastian Thomas and Mathieu Amiraux and James Baeder, University of Maryland, College Park

 

A High Deflection Diaphragm Concept (HDD) for Power Transmission Shafting
J.A. Stocco, Lucas Aerospace Power Transmission Corp.

 

A High Fidelity Brownout Model for Real-Time Flight Simulations and Trainers
Dorsett, Michael; Gilmore, Phillip; Keller, Jeffrey; McClure, Kevin; Wachspress, Daniel; Whitehouse, Glen; Yu, Ke

 

A High Fidelity Simulation Model for Comprehensive Analysis of Rotorcraft Towing Operations
He, Chengjian; Xin, Hong

 

A High-Order, Time Invariant, Linearized Model for Application to HHC/FCS Interaction Studies
Celi, R.; Cheng, R.; Tischler, M.

 

A Higher-Order Free-Wake Method for a Helicopter Rotor in Forward Flight Using Distributed Vorticity Elements
Tenzin Choephel and Mark D. Maughmer, The Pennsylvania State University

 

A Higher-Order, Free-Wake Method Applied to the Problem of Hovering Rotors
Tenzin Choephel and Sven Schmitz and Mark Maughmer, Pennsylvania State University

 

A Historical Investigation of the Mission Requirements and Enabling Technologies Influencing the Development of Unmanned Rotary-Wing Aircraft
Jason Pereira, Avericon, LLC; Scott Bruce, UASX

 

A Historical Perspective on the Application of Autonomy in Rotorcraft
Angelo Collins, CENTRA Technology, Inc. and Mary Cummings, Office of Naval Research

 

A Historical Survey of Operational Effectiveness in Relation to Preliminary Design
Robert Scott, US Army

 

A History Of Individual Flying Platforms
Jeffery A. Schroeder, NASA Ames

 

A History of Rotorcraft Comprehensive Analyses
Wayne Johnson, NASA

 

A Holistic Approach to Support
R.M. Devin, McDonnell Douglas Helicopter Co.

 

A Hybrid CFD Method for Coaxial Rotor Performance Prediction in Forward Flight
T. Egolf, Sikorsky Aircraft Corporation; N. Rajmohan, Georgia Institute of Technology; E. Reed, Sikorsky Aircraft Corporation; L. Sankar, Georgia Institute of Technology

 

A Hybrid CFD Method for Helicopter Rotors with Mesh Deformation
Chunhua Sheng, Xingyuan Su, and Qiuying Zhao, The University of Toledo; John Bridgeman and Jim Narramore, Bell Helicopter Textron

 

A Hybrid Knowledge-Based Approach To AH-64A Fault Isolation
Brian P. Millett and Richard K. Maby, McDonnell Douglas Helicopter Company

 

A Hybrid Solver with Combined CFD and Viscous Vortex Particle Method
Chengjian He, Advanced Rotorcraft Technology, Inc.; Jinggen Zhao, Advanced Rotorcraft Technology, Inc.

 

A Knowledge-Based Simulation Solution To A Heliborne Assault Force Problem
Howard R. Smith and Stuart D. Kershner, United Technologies

 

A Large-Scale Active-Twist Rotor
Anderson, David M.; Bussom, Richard C.; Mathew, Mathew B.; Weems, Douglas B.

 

A Laser Velocimetric Investigation Of The Airloads And Performance Of A Model Helicopter Rotor In Hover
J. Ramos, M. Nsimba, E. Berton, D. Favier, C.N.R.S.; M. Silva, Ames Research Center

 

A Lightweight Doppler Navigation System
Robert E. Chapman

 

A Linearized Theory for the Estimation of Helicopter Rotor Characteristics at Advance Ratios Above 1.0
Peter J. Arcidiacono, David S. Jenney and Arthur F. Smith, Research Laboratories, United Aircraft Corp.

 

A Look Back at the 1974 AHS/NASA Ames Specialists’ Meeting and the Rotor Loads Comparison
Robert A. Ormiston, U.S. Army

 

A Look Back at the 1974 AHS/NASA Ames Specialists’ Meeting and the Rotor Loads Comparison
Robert A. Ormiston, U.S. Army

 

A Low Cost, High Performance VTOL For The General Aviation Marketplace
R.L Barrie, H.M. Howell, S.J. Labows, T.C. Lund, R.D. Weissenfels, E.R. Wood, and M.A. Couch, Naval Postgraduate School

 

A Management Process for CALS Compliant Automation
G.B. Webster and R.A.M. White, McDonnell Douglas Helicopter Co.

 

A Maneuvering Flight Noise Model for Helicopter Mission Planning

Eric Greenwood, NASA Langley Research Center; Benjamin May and Christopher Hobbs, Wyle; Robert Rau, NASA Langley Research Center

 

A Manual-Control Approach to Development of VTOL Automatic Landing Technology
J. Kelly, NASA, Langley, Hampton, Va.

 

A Markov Decision Process Approach to Human/Machine Function Allocation in Optionally Piloted Vehicles
Funk, H.; Goldman, R.; Miller, C.

 

A Mechanical Speed Control for Helicopter Power Plants
Norman C. Olson

 

A Method for Determining the Fully Coupled Aeroelastic Response of Helicopter Rotor Blades
Edward R. Wood, and Kurt D. Hilzinger, Sikorsky Aircraft Div.

 

A Method for Generalized Prognostics of a Component Using Paris Law
Bechhoefer, Eric

 

A Method for Predicting Helicopter Wake Geometries, Wake-Induced Flow and Wake Effects on Blade Loads
S. G. Sadler, RASA

 

A Method for Predicting the Noise of a Tip-Jet Driven Rotor
Brentner, Kenneth; Lopes, Leonard; Morris, Philip

 

A Method for Smart Hydraulic Landing Gear Modeling and Simulation With Experimental Validation
Bryan Pilati, U.S. Army AATD, Ken-An Lou, ArmorWorks Enterprise, LLC, Phil Schaefer, Vortant Technologies, LLC, Richard Zimmerman, Zerad, LLC.

 

A Method Of Determining Safe Service Life For Helicopter Components
Gerald W. McCloud, Bell Helicopter

 

A Method Of Determining Safe Service Life For Helicopter Components
Gerald W. McCloud, Bell Helicopter

 

A Method of Qualitative Analysis During Conceptual Design as Applied to Unmanned Aerial Vehicles
Collins, Kyle B.; Mavris, Dimitri N.; Schrage, Daniel P.

 

A Method of Reducing Blade Sailing Through the Use of Trailing Edge Flaps
Jones, Mark; Newman, Simon

 

A Method to Determine Maximum Flight Control Authority Through Hardover Failure Testing
Christensen, Kevin; Hollifield, Pat; Koelzer, Helmuth; Olmstead, Michael; Wiggins, Les

 

A Method to Identify Helicopter Hover Ceiling in OGE
Chen, Renliang; Xi, Huabin; Gu, Weiyan; Yu, Xiemei

 

A Method to Integrate Drive System Design
Sylvester Ashok, Fabian Zender, Apinut Sirirojvisuth and Daniel Schrage, Georgia Institute of Technology

 

A Methodology for Rotorcraft Brownout Mitigation Through Flight Path Optimization
John Tritschler, Roberto Celi and J. Gordon Leishman, University of Maryland

 

A Methodology for Rotorcraft Brownout Mitigation Using Rotor Design Optimization
Celi, Roberto; Leishman, J.; Syal, Monica; Tritschler, John

 

A Microstrip Rotorblade Radar
Lester H. Kosowsky, L.H. Kosowsky and Associates, Inc.; Joel Walker, Malibu Research Associates, Inc.

 

A Mid-Point Evaluation Of The Rotorcraft Pilot's Associate
Rick Esquibel and Scott Swinsick, McDonnell Douglas Helicopter Systems; Keith Arthur, US Army

 

A Mid-Point Evaluation Of The Rotorcraft Pilot's Associate
Rick Esquibel and Scott Swinsick, McDonnell Douglas Helicopter Systems; Keith Arthur, US Army

 

A Miscellany of Western European V/STOL Concepts Of The 20th Century
Michael J. Hirschberg, CENTRA Technology, Inc.; Thomas Müller, Aviation Historian

 

A Modal-Based Procedure for Efficiently Predicting Low Vibration Rotor Designs
W.H. Weller and M.W. Davis, United Technologies Research Center

 

A Modal-Based Procedure for Efficiently Predicting Low Vibration Rotor Designs
W.H. Weller and M.W. Davis, United Technologies Research Center

 

A Model Following Controller Optimized for Gust Rejection During Shipboard Operations
Bridges, Derek; Horn, Joseph

 

A Model Rotor Validation for the CCR Technology Demonstrator
Joseph B. Wilkerson and Drew W. Linck, Naval Ship R&D Center

 

A Model to Simulate Rotorcraft-induced Brownout
Haehnel, Robert; Moulton, Marvin; Steinhoff, John; Wenren, Yonghu

 

A Model-based Health Monitoring and Diagnostic System for the UH-60 Helicopter
Ann Patterson-Hine, NASA Ames Research Center; William Hindson, NASA Ames Research Center; Dwight Sanderfer, NASA Ames Research Center; Somnath Deb, Qualtech Systems, Inc.; Charles Domagala, Qualtech Systems, Inc.

 

A Model-based System of Systems Engineering Distributed Package Delivery Discrete Event Simulation for Optimization of Small UAVs
Benjamin England, Atipat Wattanuntachai, Christopher Duffy, Daniel Schrage, Georgia Institute of Technology

 

A Modeling Methodology for Manned and Manned and Unmanned Aircraft in a Close Airspace Environment
Schrage, D.; Stringer, D.

 

A Modular Approach to Model Oscillating Control Surfaces using Navier-Stokes Equations
Guru P. Guruswamy, NASA Ames

 

A Modular Approach to Model Oscillating Control Surfaces using Navier-Stokes Equations
Guru P. Guruswamy, NASA Ames

 

A Modular Flight Control and Navigation System for the Next Generation of Army Aviation
C.T. Bye, J.T. Bakken and S.I. Snyder, Honeywell, Inc

 

A Modular, Networked Data Acquisition System for Airborne Applications
King, Robert; Partain, Jeremy

 

A Multi-Disciplinary Rotorcraft Simulation Facility Composed of Commodity Components and Open Source Software
Brentner, Kenneth S.; Bridges, Derek O.; Horn, Joseph F.; Lopes, Leonard V.; Sharma, Charu

 

A Multibody Formulation for Three Dimensional Brick Finite Element Based Parallel and Scalable Rotor Dynamic Analysis
Datta, Anubhav; Johnson, Wayne

 

A Multibody Study in Single- and Multi-Variable Control Algorithms for Tiltrotor Whirl Flutter Stability Augmentation
J. Mueller, R. Ferrer, T. Krysinski, Eurocopter-France; Y. Gourinat, B. Kerdreux, ENSICA

 

A Multidisciplinary Research Approach to Rotorcraft Health and Usage Monitoring
P. W. Stevens, D. L. Hall, and E. C. Smith, Pennsylvania State University

 

A Multilayered Approach for Enhancing Rotorcraft Drive System Diagnostics
Jeremy Sheldon and David Kasper and Mark Davis, Sikorsky Aircraft Corporation

 

A Multiplexed System Using A Fiber Optic Serial Data Bus
Jack Pierce, Sperry Flight Systems

 

A Multiscale Bondline Damage Characterization and Hybrid Analysis Approach for Adhesively Bonded Composite Structures
Eugene Fang, Jim Lua, Global Engineering and Materials, Inc.; Jessica Zhang, Carnegie Mellon University; Anisur Rahman and Nam Phan, Naval Air Warefare Center (PAX)

 

A Navier-Stokes/Full Potential/Free Wake Method For Advancing Multi-Bladed Rotors
Mert E. Berkman and Lakshmi N. Sankar, Georgia Institute of Technology; Charles R. Berezin and Michael S. Torok, Sikorsky Aircraft Corporation

 

A Networked Simulation Environment for Dynamic Interface Flight Control Design and Evaluation
Keller, Jeffrey; McKillip, Jr., Robert

 

A Neural Network for the Identification of Measured Helicopter Noise
R.H. Cabell, C.R. Fuller and W.F. O'Brien, Virginia Polytechnic Institute

 

A New Aerorodynamic and Acoustic Computation Chain for BVI Noise Prediction in Unsteady Flight Conditions
Costes, Michel; Perez, Guillaume

 

A New Approach To Active Control
Friedrich K. Straub and Bruce D. Charles, McDonnell Douglas Helicopter Systems

 

A New Approach to Hazard Analysis for Rotorcraft
Blake Abrecht, USAF; Dave Arterburn, University of Alabama in Huntsville; David Horney and Jon Schneider, M.I.T.; Brandon Abel , USAF; Nancy Leveson, M.I.T.

 

A New Approach to Helicopter Maintenance Development
Brian Jenkins, Bell Helicopter Textron Canada

 

A New Approach to Helicopter Maintenance Development
Brian Jenkins, Bell Helicopter Textron

 

A New Approach to Helicopter Maintenance Development
Brian Jenkins, Bell Helicopter Textron

 

A New Approach To Helicopter Stability
F. A. Erickson

 

A New Approach to the Free Wake Problem for Hovering Rotors
D.B. Bliss, D.A. Wachspress, Continuum Dynamics Inc. and Todd R. Quackenbush, Princeton University

 

A New Approach To Vulnerability Assessment Applied To Longbow Apache
Paula R. Rennaker and Steve Richardson, McDonnell Douglas

 

A New Class of Hygrothermally Stable Laminates with Extension-Twist Coupling
Armanios, Erian; Carey, Ryan; Haynes, Robert

 

A New Concept In Supercritical Drive Systems For Advanced Rotorcraft
J. E. Brunken, Bell Helicopter Textron, Inc.

 

A New Finite-Difference Method for General Long-Range Rotorcraft Acoustics: Initial Comparisons with Intermediate-Range Data
Andrew Wilson and John Steinhoff and Subhashinni Chitta, Wave CPC Inc; Ben Sim and Frank Caradonna, U.S. Army Aviation Development Directorate; Lakshmi Sankar, Georgia Tech

 

A New Formulation for Lifting Rotor Performance Including Comparison with Full-Scale Data
Ormiston, Robert

 

A New High-Speed, High-Cycle, Gear-Tooth Bending Fatigue Test Capability
David Stringer, US Army; Andrew Zakrajsek, Purdue University; Brian Dykas, Army Research Lab; Kelsen LaBerge, Army Research Lab; Robert Handschuh, NASA Glenn Research Center

 

A New Look at Lightweight Energy Absorbing Devices for Heavy Cargo Restraints
Bakis, Charles; Hagon, Matthew; Smith, Edward; Yukish, Michael

 

A New Main Rotor for the Sikorsky S-61
Curtiss, Jr., H. C.; Carson, Frank; Hill, Jeff; Quackenbush, Todd

 

A New Method for Estimating Turbulent Vortex Flow Properties from Stereoscopic DPIV Measurements
Huismann, Tyler; Johnson, Bradley; Leishman, Gordon; Ramasamy, Manikandan

 

A New Methodology for Determining the Optimal Rotational Speed of a Variable RPM Main Rotor/Turboshaft Engine System
Andrea Garavello, Hit09 S.r.l., Gianluigi Misté and Ernesto Benini, University of Padova, Maria Gonzalez-Alcoy, University of Madrid

 

A New Methodology to Predict and Optimize Rotorcraft Structural Loads/Weights Using Finite Element Method

Sohan Singh and David R. Lindsay, Bell Helicopter Textron

 

A New Methodology to Predict and Optimize Rotorcraft Structural Loads/Weights Using Finite Element Method
Sohan Singh and David R. Lindsay, Bell Helicopter Textron Inc.

 

A New Model of Rotor Dynamics During Pitch and Roll of a Hovering Helicopter
Aviv Rosen, Ahrun Isser, Technion - Israel Institute of Technology

 

A New Numerical Method for Predicting Aero-Mechanical Behaviors of A Rotor Hovering at Close Proximity to Inclined Flat Surface
N. Itoga, The National Defense Academy; T. Nagashima, The National Defense Academy; N. Iboshi, The National Defense Academy; Y. Yoshizawa, University of Tsukuba; J. V. R. Prasad, Georgia Institute of Technology; H. Xin, Georgia Institute of Technology; D. A. Peters, Washington University

 

A New Technique for Steep Angle Approach Guidance
Francis X. Kelly, Jr., Airborne Instruments Laboratory

 

A New Transonic Airfoil Design Method and Its Application to Helicopter Rotor Airfoil Design
J.C. Narramore & J.G. Yen, Bell Helicopter Textron

 

A New Unsteady Aerodynamic Model of the Coupled Rotor-Body Dynamics
A. Rosen and A. Isser, Technion - Israel Institute of Technology

 

A New VTOL UAV Cyclocopter with Cycloidal Blades System
Kim, Seung Jo; Yun, Chul Yong; Park,Illkyung; Lee, Ho Yong; Jung, Jai Sang; Hwang, In Seong; Jung, Sung Nam

 

A New, Flexible, Approach to Flight Data Acquisition
Batcheller, David

 

A Non-Linear Indicial Method for the Calculation of Unsteady Airloads
Baeder, James; Lee, Dongwook; Leishman, John

 

A Nonlinear Analysis Methodology for the Design of Skid Landing Gear
L.C. Williams and A.O. Bolukbasi, McDonnell Douglas Helicopter Co.

 

A Novel Computational Approach to High Fidelity Wind Turbine Flow Simulation
Eliot Quon and Marilyn Smith, Georgia Institute of Technology, Glen Whitehouse, Continuum Dynamics, Inc.

 

A Novel Configuration-Driven Data Mining Framework for Health and Usage Monitoring Systems
Al-Kateb, Mohammed; Bechhoefer, Eric; He, David; Imadabathuni, Mahindra; Joshi, Pradnya

 

A Novel Gear Condition Monitoring Method Based on Transient Impulse Response
Paula Dempsey, NASA Glenn Research Center; Yan Chen and Zaffir Chaudhry, United Technologies Research Center

 

A Novel Instrumentation System for Measurement of Helicopter Rotor Motions and Loads Data
McKillip, Robert, Jr.

 

A Novel Parallel Algorithm for Rotor Dynamics Simulation
Olivier Bauchau, University of Michigan-Shanghai Jiao Tong University Joint Institute; Seundo Heo, Georgia Institute of Technology

 

A Novel, High Fidelity 6-DoF Simulation Model for Tethered Load Dynamics
Daniel Prosser and Marilyn Smith, Georgia Institute of Technology

 

A Numerical Analysis of the British Experimental Rotor Program Blade
E.P.N. Duque, U.S. Army Aeroflightdynamics Dir.

 

A Numerical and Experimental Investigation of Electrothermal Aircraft Deicing
K.L. Leffel, K.C. Masiulaniec, K.J. DeWitt and T.G. Keith, Jr., University of Toledo

 

A Numerical Investigation of Ground Effect on a Coaxial Rotor System
Mark Dreier and Ashley Paredes, AVX Aircraft Company

 

A Numerical Optimization of Lightweight Multilayer Armour
Andrea Manes and Marco Giglio, Politecnico Di Milano

 

A Numerical Study of Advanced Rotor Blades
G. Abdy and V. Wells, Arizona State University

 

A Numerical Study of Advanced Rotor Blades
G. Abdy and V. Wells, Arizona State University

 

A Numerical Study of Advanced Rotor Blades
G. Abdy and V. Wells, Arizona State University

 

A Numerical Study of Sand Particle Distribution, Density and Sand Shape Effects on the Scavenge Efficiency of Engine Inlet Particle Separator Systems
Taslim, M.E.; Spring, Samuel D.; Tingle, Walter J.; Oliver, Wayne.R.

 

A Numerical Study of Sand Separation Applicable to Engine Inlet Particle Separator Systems
Khanicheh, A; Oliver, W. R.; Spring, S. D.; Taslim, M. E.

 

A Parameter Identification Method for Helicopter Noise Source Identification and Physics-Based Semi-Empirical Modeling
Greenwood, Eric; Schmitz, Fredric

 

A Parametric Analysis Method for Rotor Blade Structural Design
Alex Berman

 

A Parametric Design Study for a Swashplateless Helicopter Rotor with Trailing-Edge Flaps
Shen, Jinwei; Chopra, Inderjit

 

A Parametric Study for a Structural Intensity based Damage Detection Technique
Fabio Semperlotti, Walter T. Schmidt, Edward C. Smith, Stephen C. Conlon and Jeffrey C. Banks, The Pennsylvania State University

 

A Parametric Study of Blade/Vortex Interaction For Two, Three and Four-Bladed Model Rotors at Moderate Tip Speeds: Theory and Experiment
K.P. Leighton & W.L. Harris, Massachusetts Institute of Technology

 

A Parametric Study Of Harmonic Rotor Hub Loads
Cheng-Jian He, Lockheed Engineering and Sciences Company

 

A Parametric Study of On-Blade Control Device Performance for Helicopter Vibration and Noise Reduction
Ashwani Padthe and Peretz Friedman and Miang Chia, University of Michigan

 

A Parametric Study of Real Time Mathematical Modeling Incorporating Dynamic Wake and Elastic Blades
C. He and W.D. Lewis, Georgia Institute of Technology

 

A Parametric Study of the Structural Design for an Advanced Active Twist Rotor
Martin K. Sekula, Matthew L. Wilbur, William T. Yeager, Jr., NASA Langley Research Center

 

A Performance Analysis of Compound Helicopter Configurations
Kevin Ferguson and Douglas Thomson, University of Glasgow

 

A Performance Based Optimization of High Speed Prop-Rotors
Thomas McCarthy, Aditi Chattopadhyay, Arizona State University; Peter D. Talbot and John F. Madden, III, NASA Ames

 

A Perspective Of Future Rotorcraft Technology
P.N. Goddard, GKN Westland Helicopters Limited

 

A Physics-Based Approach to Trim Optimization of an Articulated Slowed-Rotor Compound Helicopter in High-Speed Flight
Jean-Paul Reddinger and Farhan Gandhi, Rensselaer Polytechnic Institute

 

A Physics-Based Approach to Trim Optimization of Coaxial Helicopters in High-Speed Flight
George Jacobellis and Farhan Gandhi, Rensselaer Polytechnic Institute; Matthew Floros, U.S. Army Research Laboratory

 

A Physics-Based Hydraulic Damper Model for Rotor Structural Loads
Hao Kang and Matt Floros, US Army Research Laboratory; Jean-Pual Reddinger, Rensselaer Polytechnic Institute

 

A Physics-Based Investigation of Gurney Flaps for Rotor Vibration Reduction
Min, Byung-Young; Prasad, JVR; Sankar, Lakshmi; Schrage, Daniel

 

A Physics-Based Model of Rotorcraft Brownout for Flight Simulation Applications
J.D. Keller, G.R. Whitehouse, D.A. Wachspress, M.E. Teske, T.R. Quackenbush, Continuum Dynamics, Inc.

 

A Pilot's Opinion: VTOL Control Design Requirements for Instrument Approach Task
J. M. Patton, Jr. NASA Langley Research Center

 

A Pilot's Perspective of Automated Mission Management
D.R. Bailey and N.J. Pekelsma, TAU Corporation

 

A Piloted Simulation Investigation of Pitch and Roll Handling Qualities Requirements for Air-to-Air Combat
M.S. Whalley, U.S. Army Aeroflightdynamics Directorate, and W.R. Carpenter, Sterling Federal Systems, Inc.

 

A Piloted Simulation Investigation of Yaw Dynamics Requirements for Turreted Gun Use in Low-Level Helicopter Air-to-Air Combat
W.A. Decker, NASA Ames Research Center, P.M. Morris, Sikorsky Aircraft Division, UTC, and J.N. Williams, USA

 

A Piloted Simulation of One-on-One Helicopter Air Combat at NOE Flight Levels
M.S. Lewis, U.S. Army Aviation Systems Command Research and Technology Laboratories

 

A Piloted Simulation of One-on-One Helicopter Air Combat at NOE Flight Levels
M.S. Lewis, U.S. Army Aviation Systems Command Research and Technology Laboratories

 

A Piloted Simulation of the Backup Control System Engagement for the YAH-64
C. Blanken, E. Aiken & LTC R. Merrill, U.S. Army Aeromechanics Laboratory, & V. Ross, NASA Ames Research Center

 

A Piloted Simulator Investigation of Augmentation Systems to Improve Helicopter Nap-of-the-Earth Handling Qualities
Chen, Robert T. N., Rotorcraft Flight Dynamics; Talbot, Peter D.; Gerdes, Ronald M., NASA; Dugan, Daniel C., NASA

 

A Piloted Simulator Investigation of Decoupling Helicopters by Using a Model Following Control System
G. Bouwer, DFVLR and K.B. Hilbert, U.S. Army Research and Technology Laboratories (AVSCOM)

 

A Piloted Simulator Investigation of Side-Stick Controller/Stability and Control Augmentation System Requirements for Helicopter Visual Flight Tasks
K.H. Landis & P.J. Dunford, Boeing Vertol Company and E.W. Aiken & K.B. Hilbert, U.S. Army Aeromechanics Laboratory

 

A Playbook Approach to Variable Autonomy Control: Application for Control of Multiple, Heterogeneous Unmanned Air Vehicles
Funk, Harry B.; Goldman, Robert P.; Miller, Christopher A.; Pate, Billy B.; Wu, Peggy

 

A Portable Display for Evaluating Handling Qualities in Shipboard Hover
Dave Mitchell, Mitchell Aerospace Research; Sean Roark and Gino Molinaro, US Navy (NAVAIR)

 

A Portable Mission Performance and Planning Computer System for Military Helicopter Operations
K.A. Stanzione and R.F. Smith, Praxis Technologies Corp.

 

A Possible Personality Trait Variable in the Prediction and Measurement of Operator Workload
J.S. Seeman, McDonnell Douglas Helicopter Systems

 

A Power Assurance Algorithm For Continuous, Near Real Time, In-Flight Monitoring Of Aircraft Engine Performance
Richard Ling and Grant Gordon, Honeywell

 

A Practical Approach to Obstacle Field Route Planning for Unmanned Rotorcraft
Howlett, Jason K.; Mansur, M. Hossein; Schulein, Greg

 

A Practical Approach to Rotorcraft Systems Identification
R.W. DuVal, Advanced Rotorcraft Technology, Inc. and J.E. Wang & M. Demiroz, San Jose State University

 

A Practical Approach to the Metal Blade Spar Problem
F. L. Stulen and A. J. Belfour

 

A Practical Regime Prediction Approach for HUMS Application
Bechhoefer, Eric; He, David; Wu, Shenliang

 

A Precision Flight Test Application of a Differential Global Positioning System
M. Hardesty, M. Metzger, and J. Flint, McDonnell Douglas Helicopter Systems

 

A Preliminary Analysis Of Indicated Torque Response Requirements For Aggressive Helicopter Heave Axis Handling
Robert Erdos, National Research Council of Canada; Kris Ellis, National Research Council of Canada

 

A Preliminary Flight Investigation of Cross-Coupling and Lateral Damping for Nap-Of-The-Earth Helicopter Operations
L. Corliss & G. Carico, U.S. Army Aeromechanics Laboratory

 

A Preliminary Investigation of the Handling Qualities of the Bell 412 HP Helicopter During Flight Using Night Vision Goggles
Stewart W. Baillie, J. Murray Morgan, Research National Research Council Canada

 

A Prescribed Wake Lifting Surface Hover Performance Analysis
J. David Kocurek; James L. Tangler

 

A Pressurized Spar Inspection System
Thomas P. Dixon, Sikorsky Aircraft Div.

 

A Principled Approach to Enable Safe and High Performance Maneuvers for Autonomous Rotorcraft
Sanjiban Choudhury and Sankalp Arora and Sebastian Scherer and Daniel Althoff, Carnegie Mellon University

 

A Probabilistic Approach for Reliability Quantification of Propulsion Materials
Michael Shiao, Tzikang Chen, Anindya Ghoshal, Department of Army

 

A Probability-Based Approach to Helicopter Track and Balance
Danai, K.; Wang, S.

 

A Probablistic Method of Risk Assessment in Terms of Meeting Design Goals
Daniel B. Robertson, John P. Magee, Bell Helicopter Textron, Inc.

 

A Procedure For the Adjustment of the Endurance Limit of a Component To Account For a Reduction in the Number of Fatigue Test Specimens
W.D. Harris, Hughes Helicopters, Inc.

 

A Program for Increased Flight Fidelity in Helicopter Simulation
LT C. W. Woomer, USN, and G. D. Carico

 

A Promising New Vertical Take-Off and Landing (VTOL) Aircraft Concept
J. Lawrence, Lawrence Engineering

 

A Prospective: The Importance of Propulsion Technology to the Development of Helicopter Systems With a Vision for the Future
Kenneth M. Rosen, PhD, Aero-Science Technology Associates, LLC

 

A Qualitative Examination of Dynamic Stall from Flight Test Data
William G. Bousman, U. S. Army ATCOM

 

A Qualitative Flight Evaluation of a Sidestick Controller in the XV-15 Tiltrotor Research Aircraft
Daniel C. Dugan, NASA Ames; Gary C. Churchill, US Army AMCOM

 

A Rapid Geometry Generator for Rotorcraft Exploratory Design with Computational Fluid Dynamics
Hirsh, Joel; Narducci, R.

 

A Ray Acoustics Approach to Fuselage Scattering of Rotor Noise
N. Attalla and S.A.L. Glegg, Florida Atlantic University (AIAA Exchange Paper)

 

A Re-Configurable Portable Simulator to Support Rotorcraft Tactical Mission Rehearsal and Advanced Concepts Prototyping
Brychcy, Michael; Lamont, Rebecca; Margetich, Stephen; Redkoles, Paul; Seals, Rupert; Taylor, James

 

A Real Time Expert Control System for Helicopter Autorotation
Jonathan Rogers, Georgia Institute of Technology; Zachary Sunberg and Nate Miller, Texas A&M University

 

A Real Time Finite State Induced Flow Model Augmented with High Fidelity Viscous Vortex Particle Simulation
He, Chengjian; Zhao, Jinggen

 

A Redesigned Tail Rotor for Improvement of CH-53E High-Altitude Performance
Pritchard, James A.; Kunz, Donald L.

 

A Redundant Aircraft Attitude System Based on Fuzzy Logic Data Fusion of the Miniaturized Inertial Sensors
Dragos George Sandu, In Flight Research and Test Center Craiova; Ruxandra Mihaela Botez, Ecole de Technologie Superieure; Teodor Lucian Grigorie, University of Craiova

 

A Refined Beam Theory For Advanced Composite Rotor Blade Analysis
J. B. Kosmatka, Virginia Polytechnic Institute and State University

 

A Report On The Heliport Environment
Arthur L. Fornoff, Bell Helicopter Company

 

A Research Program for Helicopter Noise Reduction
Kobiki Noboru, Atsushi Murashige, Yasumichi Hasegawa, Tomoka Tsujiuchi, Natsuki Kondo, Hiroki Nishimura, Akio Ochi, Kawasaki

 

A Retrospective Of 3600 Composite Blades
C.P. Hardersen and P.F. Maloney, Kaman Aerospace Corporation

 

A Retrospective Survey of Pilot-Structural Coupling Instabilities in Naval Rotorcraft
Walden, Ronald

 

A Review of Advanced Rotor Research
M.W. Kelly and J.P. Rabbott

 

A Review of Current Finite Difference Rotor Flow Methods
F.X. Caradonna and C. Tung, U.S. Army Aeroflightdynamics Directorate

 

A Review of Current Helicopter Loads Research As Applied to the Problem of Rotor-Blade Fatigue Substantiation
John F. Ward and LeRoy H. Ludi

 

A Review of Design Objectives for Advanced Helicopter Rotor Airfoils
Leo U. Dadone and Toshiyuki Fukushima, Boeing Vertol Company

 

A Review Of Dynamic Inflow And Its Effect On Experimental Correlations
Gopal H. Gaonkar, Indian Institute of Science; David A. Peters, Washington University

 

A Review of MIL-F-83300 for Helicopter Applications
D. L. Green, PACER Systems, Inc.

 

A Review of the Motion Picture "Los Angeles Airways Operations"
Short, V. R., Sikorsky Aircraft

 

A Review of the V-22 Dynamics Validation Program
J.E. Brunken, Jr., D.A. Popelka, and R.J. Bryson, Bell Helicopter Textron

 

A Review of the V-22 Health Monitoring System
M.J. Augustin and G.D. Middleton, Bell Helicopter Textron

 

A Review Of Turbine Engine Vibration Criteria For VTOL Aircraft
R.W. Ba1ke, Bell Helicopter Company

 

A Revolutionary Control Framework for UAVS and Other Embedded Systems
Koenig, William; Mendel, Brian; Paunicka, James

 

A Rigid Body Model for Analysis of Aerogenerator Rotor Dynamics
C. E. Smith, R. W. Thresher, R. E. Wilson, and R. B. MacDuff, Oregon State University

 

A Rip Van Winkle Programmatic View of Rotary Wing Aeronautics: 1996-2008
Walls, Anser

 

A Roll-Lateral Helicopter Side-Step Maneuver on the MPI Motion Simulator
Beykirch, Karl; B?lthoff, Heinrich; Nieuwenhuizen, Frank; Nusseck, Hans-G?nther; Teufel, Harald

 

A Rotor Tip Vortex Tracing Algorithm for Image Post-Processing
Austin Overmeyer, U.S. Army ADD/AFDD

 

A Rotorcraft Adaptation of Geneva Aerospace's Variable Autonomy Control System
Pate, Billy B.

 

A Rotorcraft Aerodynamics CFD Solution Method Based Vorticity Confinement
Chitta, Subhashini; Steinhoff, John; Wachspress, Daniel; Wenren, Yonghu

 

A Round Robin Exercise to Assess Capability Topredict Crack Growth Lives and Inspection Intervals for Damage Tolerant Design in Helicopters
Bristow, J.; Irving, P.; Lin, J.

 

A Safe and Fuel-Efficient VTOL "Personal Aircraft"
Milde, Jr., Karl; Pruszenski, Jr., Anthony; Wagner, Joseph

 

A Satellite Data Link for HUMS Applications
Buckley, S.; Haas, D.; Natoli, L.

 

A Scalable and Adaptive Approach to Data Fusion for Autonomous UAVs
J. Rosswog, R. Szczerba, Lockheed Martin Systems Integration; K. Ghose, State University of New York at Binghamton

 

A Scientific Approach to Spares Prediction
Paul Nicholas, Sikorsky Aircraft

 

A Second Approximation To The Induced Drag Of A Rotor In Forward Flight
R.W. Prouty, Hughes Helicopters

 

A Self-Excited Rotor Blade Oscillation At High Subsonic Mach Numbers
William F. Paul

 

A Self-Monitored Stability Augmentation System For The CX-84 V/Stol Aircraft
C. D. Griffith; V. M. Crosby

 

A Semi-Empirical Correction for the Vortex Core Effect on Hovering Rotor Wake Geometries,
S.S. Samant and R.B. Gray

 

A Semi-Empirical High-Speed Rotor Noise Prediction Technique
K.R. Shenoy, Bell Helicopter Textron

 

A Semi-Empirical Noise Modeling Method for Helicopter Maneuvering Flight Operations
Eric Greenwood, NASA Langley Research Center and Fredric Schmitz and Richard Sickenberger, University of Maryland

 

A Sequential Shifting Algorithm for Variable Rotor Speed Control
DeCastro, Jonathan; Edwards, Jason; Litt, Jonathan

 

A Simple Elasticity Solution For Predicting Interlaminar Stresses In Composite Flexbeams
Andrew Makeev, Georgia Institute of Technology; Erian A. Armanios, Georgia Institute of Technology

 

A Simple Method for Determining Service Limits for Damage Tolerant Electrothermal Heaters
David Lawson, AlliedSignal Aerospace Canada; Marian Nemec, University of Toronto

 

A Simple Method for Determining Service Limits for Damage Tolerant Electrothermal Heaters
David Lawson, AlliedSignal Aerospace Canada; Marian Nemec, University of Toronto

 

A Simple Short-Term Solution to Helicopter Spatial Disorientation During Operations in Degraded Visual Environments
Angus Rupert and John Ramiccio, USAARL; Braden McGrath, University of Canberra; Joe McKay, AED AMRDEC; Sergey Drakunov, Embry-Riddle Aeronautical University

 

A Simplified Approach To Generalized Helicopter Configuration Modeling And The Prediction Of Fuselage Surface Pressures
Thomas W. Sheehy, Sikorsky Aircraft

 

A Simplified Empirical Method For Rotor Component Fatigue Design
G. L. Garham; M. J. McGuigan

 

A Simplified Inflow Model of a Helicopter Rotor in Vertical Descent
Basset, Pierre-Marie; Chen, Chang; Prasad, J.V.R.

 

A Simplified Study of High Speed Autorotation Entry Characteristics
H. H. McIntyre, Kaman Aerospace Corp.

 

A Simplified Theory of Hingeless Rotors with Application to Tandem Helicopters
Dr. M. I. Young

 

A Simulation Assessment of the Westland Lynx Stability and Command Augmentation System for Air-to-Air Tracking Tasks
J. Howitt, Defense Research Agency

 

A Simulation Model of Ship Ground Effect for Rotorcraft/Ship Interaction Study
Hong Zhang, O.A.F. Mello, J.V.R. Prasad, Georgia Institute of Technology; L.N. Sankar, John D. Funk, Jr., Naval Air Warfare Center Aircraft Division

 

A Simulation Model to Investigate the Impact of Health and Usage Monitoring Systems (HUMS) on Helicopter Operations and Maintenance
Schaefer, Carl G., Jr.; Haas, David J.

 

A Skin-Stringer Design for a Crashworthy Composite Fuselage for the Hughes 500E Helicopter
J.K. Sen and M.W. Votaw, Hughes Helicopters Inc

 

A Smart Position Sensor for Articulated Rotors
Troy Schank and Kynn Schulte, Bell Helicopter Textron Inc; 

 

A Special Gas Turbine Cycle For The Compound Helicopter
J. B. Nichols

 

A State-Of-The-Art Survey Of Two-Dimensional Airfoil Data
R.W. Prouty, Hughes Helicopters

 

A State-Space Airloads Theory for Flexible Airfoils
D. Peters, McDonnell Douglas Professor of Engineering; M.-C.A. Hsieh, Washington University; A. Torrero, Parks College of Aeronautics, St. Louis University

 

A State-Space Free-Vortex Hybrid Wake Model For Helicopter Rotors
Bryan J. Wasileski, Charles Stark Draper Laboratory; David A. Peters, Washington University in St. Louis

 

A Statistical Turbulence Model for Shipboard Rotorcraft Simulations
He, Chengjian; Xin, Hong

 

A Stochastic Model of Unsteady Ship Airwake Disturbances on Rotorcraft
Geiger, Derek; Horn, Joseph; Sahasrabudhe, Vineet; Sparbanie, Sade

 

A Stress Analysis Method To Study Surface And Structural Fatigue Of Bearing Raceway Integrated On Gears
Jean-Michel Sprauel, Aix Marseille Université, Magali Mailhé and Emmanuel Mermoz and Arnaud Delabie, Eurocopter

 

A Structured Approach For Integration And Test Of Avionics Systems
Joseph M. Medwetz, IBM Federal Systems

 

A Structured/Unstructured Embedded Grid Solver for Helicopter Rotor Flows
Earl-Peter Duque, U.S. Army Aeroflyghtdynamics Directorate, ATCOM

 

A Study in Rotor Mechanics
Bartram Kelley

 

A Study of Acoustic Reflections in Full-Scale Rotor Low Frequency Noise Measurements Acquired in Wind Tunnels
N. Barbely, Georgia Institute of Technology; B. Sim, University of California Santa Cruz; C. Kitaplioglu, NASA Ames Research Center; C. Hartley, Jacobs Technology, Inc.

 

A Study of Bearingless Rotor-Hub System for XOH-1
Yoshiyuki Niwa, The 3rd Research Center, TRD& JDA; Shun -Ichi Bandoh, Kawasaki Heavy Industry

 

A Study of Blade-Vortex Interaction Sound Generation and Directionality
Todd D. Ringler, Albert R. George, and James B. Steele, Cornell University

 

A Study of Blade-Vortex Interaction Sound Generation and Directionality
Todd D. Ringler, Albert R. George, and James B. Steele, Cornell University

 

A Study of Blade-Vortex Interaction Sound Generation and Directionality
Todd D. Ringler, Albert R. George, and James B. Steele, Cornell University

 

A Study of Coaxial Rotor Performance and Flow Field Characteristics
Natasha Lydia Barbely (NASA Ames Research Center), Narayanan M. Komerath (Georgia Institute of Technology), and Luke A. Novak (Sukra Helitek)

 

A Study of Coupled Engine/Rotor Dynamic Behavior
Ketao Liu, Manoj Mittal, J. V. R. Prasad, Christoph J. Scholz, Georgia Institute of Technology

 

A Study of Dual-Rotor Interference and Ground Effect Using a Free-Vortex Wake Model
Griffiths, Daniel A.; Leishman, John Gordon

 

A Study of Helicopter Landing Behavior on Small Ships
R. M. Tuttle, Kaman Aerospace

 

A Study of Leading Edge Shapes for the Front Duct of a Dual Ducted Fan Vehicle
Ryan Hook, The Pennsylvania State University; Leighton Myers, The Pennsylvania State University; Dennis McLaughlin, The Pennsylvania State University

 

A study of Nanoparticle Additives on the Performance of the AH-64 Intermediate Gearbox Lubricant to Achieve CBM Objectives
Kareem Gouda, Mohsen Nikhoo, Steve Marcous, Dr. Abdel-Bayoumi, Dr. Joshua Tarbutton, University of South Carolina; Kenneth Eberts and Ganesh Skandan, NEI Corporation/AED; MG. Les Eisner, SC National Guard

 

A Study of Nanoparticle Additives on the Performance of the AH-64 Intermediate Gearbox Lubricant to Achieve CBM Objectives
Kareem Gouda, Mohsen Nikhoo, Steve Marcous, Dr. Abdel-Bayoumi, Dr. Joshua Tarbutton, University of South Carolina; Kenneth Eberts and Ganesh Skandan, NEI Corporation/AED; MG. Les Eisner, SC National Guard

 

A Study Of Noise Produced By A Helicopter Rotor-Tip Vortex Interaction
W. Steve Shepard and J. R. Wolfe, Mississippi State University

 

A Study of Planar and Nonplanar Membrane Wing Planforms for the Design of a Flapping-Wing Micro Air Vehicle
B. Beasley, I. Chopra, University of Maryland

 

A Study of Rotary-Wing Crashes to Support New Crashworthiness Criteria
Labun, Lance

 

A Study of Rotor Blade-Vortex Interaction
Prof. B. W. McCormick, Jr., Pennsylvania State University; and M. Surendraiah, Segner & Dalton

 

A Study of Stall-Induced Flap-Lag Instability of Hingeless Rotors
R. A. Ormiston and W. G. Bousman, USAAMR&DL, Moffett Field, Calif.

 

A Study of the Aerodynamic Interaction Between a Main Rotor and a Fuselage
C.A. Smith & M.D. Betzina, NASA-Ames Research Center

 

A Study of the Aerodynamic Interaction Between a Main Rotor and a Fuselage
Authors: C.A. Smith & M.D. Betzina, NASA-Ames Research Center.

 

A Study of the Aerodynamics and Acoustics of Super-BVI
H.-N. Chen, K.S. Brentner, J. Shirey, J. Horn, The Pennsylvania State University; S. Ananthan, J.G. Leishman, University of Maryland

 

A Study Of The Army Standard Hot Day
William G. Bousman, U.S. Army

 

A Study of the Effects of Non-Uniform Swash-Plate Stiffness and Out-of-Blade Track on Rotor Dynamics and Stability
V. J. Piarulli, RASA

 

A Study of the HART-I Rotor with Loose Computational Fluid/Structural Dynamic Coupling
Stephen M. Makinen, Matthew Hill, Farhan Gandhi, Lyle N. Long, The Pennsylvania State University; Roxana Vasilescu, Lakshmi Sankar, Georgia Institute of Technology

 

A Study Of The Potential Benefits Of Advanced Airfoils For Helicopter Applications
Vincent M. Paglino and David R. Clark, United Aircraft Corp.

 

A Study of the Retirement Data for Rotorcraft Dynamic Components
Martin, E.; Rumph, Frederick

 

A Study of the Rotor Wake of a Small-Scale Rotor Model in Forward Flight Using Laser Light Sheet Flow Visualization with Comparisons to Analytical Models
T.A. Ghee, Analytical Services & Materials, Inc., and J.W. Elliott, U.S. Army Aerostructures Directorate

 

A Study of the Turbine Integrated Geared Rotor for the Heavy-Lift Helicopter
Robert B. Bossler, Jr., Kaman Aircraft Corp.

 

A Study of Turbine-Powered Helicopter Drive System Instability
John C. Keeling, and David L. Kidd

 

A Study on Blade Torsion Characteristics - Comparison and Evaluation of Analysis with DNW Test Results
Kobiki Noboru, Atsushi Murashige, Kawasaki Heavy Industries, Ltd.

 

A Study on Rotor Tip-Vortex Pairing Phenomena by using Time-Marching Free-Wake Method
Ki Hoon Chung, Korea Advanced Institute of Science of Technology; Seon Uk Na, Korea Advanced Institute of Science of Technology; Wan Ho Jeon, Korea Advanced Institute of Science of Technology; Duck Joo Lee, Korea Advanced Institute of Science of Technology

 

A Study To Determine The Characteristic Shapes Of Helicopter Visual Approach Profiles
Gene C. Moen; Daniel J. DiCarlo; Kenneth R. Yenni

 

A Study to Improve Flying Qualities in IMC for Civil Helicopters
Koji Amano, ATIC; Kazuhiro Kimura, ATIC; Shoji Tanase, ATIC; Ikuo Sudo, ATIC; Shuichiro Ozeki, ATIC

 

A Subjective Test of Modulated Blade Spacing for Helicopter Main Rotors
Sullivan, Brenda M.; Edwards, Bryan D.; Brentner, Kenneth S.; Booth, Earl R., Jr.

 

A Successful Comprehensive Rotor Dynamics Correlation for a Sikorsky Full-Scale Bearingless Main Rotor
James M. Wang, Sikorsky Aircraft Corp.

 

A Successful Comprehensive Rotor Dynamics Correlation for a Sikorsky Full-Scale Bearingless Main Rotor
James M. Wang, United Technologies Corporation

 

A Summary of AH-64D Apache Longbow Network Experimentation Enabled by the MCAP Embedded Architecture
Dale Lee Johnson, U.S. Army

 

A Summary of DOD-Sponsored Research Performed at NASA Langley's Impact Dynamics Research Facility
Boitnott, Richard L.; Fasanella, Edwin L.; Jackson, Karen E.; Jones, Lisa E.; Lyle, Karen H.

 

A Summary of Hingeless-Rotor Research at NASA-Langley
John F. Ward and Robert J. Huston, NASA

 

A Survey of Agile Systems Engineering Methods, Process, and Tools
Colbert, Edward; Componation, Paul; O'Brien, Sue; Sabados, Dawn; Shull, Forrest; Turner, Richard

 

A Survey of Hub Vibration for the UH-60A Airloads Research Aircraft
Karen Studebaker, NASA Ames

 

A Survey of Rotor Loads Distribution In Maneuvering Flight
Robert M. Kufeld, NASA Ames; Jeffrey L. Cross, William G. Bousman, ATCOM

 

A Survey of Variable Stability Helicopter Applications in Handling Qualities Research
J. Fletcher, U.S. Army Aeroflightdynamics Directorate, Marc Alexander, National Research Council, Canada, Marc Hoefinger, German Aerospace Research Center

 

A Swashplateless Helicopter Rotor with Trailing-Edge Flaps for UH-60 Helicopter
Jinwei Shen, Inderjit Chopra, University of Maryland

 

A Synergistic Approach to Logistics Planning and Engine Design
M.A. Hall and K.C. Ross, Light Helicopter Turbine Engine Co.

 

A System Framework for an Automated Pre-Mission Success Evaluation of Medical Emergency Service Helicopters
Sinha, A. K.; Kusumo, R.; Bourmistrova, A.; Hogan, P.; Laycock, K.

 

A System Framework Of The Design Parametric Analysis Sub-Module For Modeling Upgrade Design Analysis Of Anti-Submarine Maritime Helicopters
Srinivas Jonnalagadda, Arvind. K. Sinha, Peter Hoffmann, RMIT University; Daniel. P. Schrage, Georgia Institute of Technology

 

A System Methodology for Design Robustness Analysis of Helicopter Mid-Life Upgrades
Raden Kusumo, Arvind K. Sinha, Royal Melbourne Institute of Technology

 

A System Methodology to Define Mission Capabilities for Helicopter Emergency Medical Operations
Hogan, P.; Kusumo, R.; Laycock, K.; Momin, M.; Sinha, A.

 

A System Solution for Helicopter Nap-of-the-Earth (NOE) Communications
K. Wroblewski, McDonnell Douglas Helicopter Co., and R. Rudow, formerly with McDonnell Douglas Helicopter Co.

 

A Systematic Approach to an Advanced High Power Density Gear: PYROWEAR 675
H.A. Chin, L.D. Wedeven, S.H. Kratz, N.H. Forster, G.G. Wedeven and W.F. Black, Wedeven Associates Inc.

 

A Systematic Approach to Bearing Health Monitoring
Hickenbottom, Chris; Kim, Kyusung; Uluyol, Onder

 

A Systematic Approach to Reducing UH-60M Tail Drive Shaft Maintenance
Avinash Sarlashkar and Matthew Watson and Jeremy Sheldon and Jeffrey Steele and David Kasper and Mark Davis, Sikorsky Aircraft Corporation, Jason Fetty, U.S. Army Aviation Applied Technology Directorate

 

A Systematic Study of Helicopter Rotor Stall Using Model Rotors
A. J. Landgrebe and E. D. Bellinger, UARL.

 

A Systems Approach to Crash Protection
John Crocco, U.S. Army AATD

 

A Systems Approach to Model the Conceptual Design Process of Vertical Take Off Unmanned Aircraft Vehicle (VTUAV)
Rathore, A.; Sinha, Arvind K.

 

A Systems Approach to the Conceptual Design of a Vertical Take-Off Unmanned Combat Aerial Vehicle
Khreish, Joseph; Sinha, Arvind K.; Atyeo, Simon

 

A Systems Approach to the Design & Development of a Helicopter Fleet Management System - Phase 1 and 2
Schauenburg, Axel; Sinha, Arvind

 

A Systems Engineering Approach to Carefree Maneuvering in the BA609
King, David W.; Bianco-Mengotti, Riccardo; Fortenbaugh, R.L.; Schaeffer, Joseph M.

 

A Systems Engineering Approach to Trading Conflicting Requirements
Christine Collins, Lockheed Martin

 

A Systems Engineering Approach: Working with the Customer to Establish a Cost Effective Request for Proposal
Botta, Sebastian; Hensley, Philip

 

A Systems Engineering Approach: Working With The Customer To Establish A Cost Effective Request for Proposal
Sebastian W. Botta, Philip Hensley, Sikorsky Aircraft Corporation

 

A Systems Engineering Approach: Working With The Customer To Establish A Cost Effective Request for Proposal
Sebastian W. Botta, Philip Hensley, Sikorsky Aircraft Corporation

 

A Systems Engineering Modeling and Simulation Approach for Rotorcraft Drive System Optimization
Sylvester V. Ashok, Daniel P. Schrage, Alexander Robledo, Georgia Institute of Technology

 

A Tactics Expert System for Scout/Attack Rotorcraft
Eddie J. Trujillo, and Charles D. Holley, Bell Helicopter Textron, Inc.

 

A Taguchi Analysis of Helicopter Maneuverability and Agility
S.R. Swinsick, McDonnell Douglas Helicopter Co.

 

A Tensor-Skin Concept for Crashworthiness of Helicopters in Case of Water Impact
Hubertus C.S.J. Thuis, JaapF.M. Wiggenraad, National Aerospace Laboratory, NLR

 

A Theoretical Method for Rotor Blade Flutter in Forward Flight
K. W. Shipman, and E. R. Wood, Georgia Institute of Technology

 

A Theory for the Analysis of Rotorcraft Operating in Atmospheric Turbulence
M.F. Costello, Boeing Helicopters

 

A Thin Film Electroluminescent Display For Cockpit Applications
Gerald L. Vick, James P. Shephard, Wesley G. Runyan, James S. Trcka, Rockwell International

 

A Third Generation Energy Absorber for Crash Attenuating Helicopter Seating
Dr. Lance C Labun, Simula, Martin Rappaport, NA WC

 

A Tool for Low Noise Procedures Design and Community Noise Impact Assessment: The Rotorcraft Noise Model (RNM)
David A. Conner, U.S. Army; Juliet A. Page, Wyle Laboratories

 

A Tool for Rotorcraft Pre-Design
Sky Sartorius, Technical University of Munich

 

A Tool for Rotorcraft Pre-Design
Sky Sartorius, Technical University of Munich

 

A Toolbox for Rotorcraft Preliminary Design
Max Lier and Alex Krenik and Philipp Kunze and Dieter Kohlgrüber and Marius Lützenburger and Dominik Schwinn, German Aerospace Center (DLR)

 

A Transfer Function Method for Dynamic Stability Measurement
W. Johnson

 

A Tribute to Professor Rene H. Miller a Pioneer in Aeromechanics and Rotary Wing Flight Transportation
Peretz Friedmann, University of Michigan; Wayne Johnson, NASA Ames research Center

 

A Tunnel Spanning Airfoil Testing Technique
Dale R. Chaddock, Naval Ship Research and Development Center

 

A Unified Approach to the Optimal Design of Adaptive and Gain Scheduled Controllers to Achieve Minimum Helicopter Rotor Vibration
J. Molusis, University of Connecticut, C. Hammond, U.S. Army Applied Technology Laboratory, and J. Cline, U.S. Army Structures Laboratory

 

A Unified Control and Simulation Tool in Suppport of Rotorcraft/Ship Dynamic Interface
Chengjian He, Advanced Rotorcraft Technology, Inc.; Dooyong Lee, Advanced Rotorcraft Technology, Inc.; Jinggen Zhao, Advanced Rotorcraft Technology, Inc.; Chris Ware, Advanced Rotorcraft Technology, Inc.

 

A Unified Formulation of Rotor Load Prediction Methods
R.E. Hansford, Westland Helicopters Ltd

 

A Unified Theoretical-Computational Approach For Viscous Unsteady Rotor Aerodynamics
Dr. J.C. Wu and I.H. Tuncer, Georgia Institute of Technology

 

A Unifying Approach for Rotor-craft Information Systems
Amulya K. Garga, The Pennsylvania State University; David L. Hall, The Pennsylvania State University

 

A USN Strategy for Mechanical and Propulsion Systems Prognostics with Demonstration Results
Hardman, William; Hess, Andrew

 

A Variable Diameter Short Haul Civil Tiltrotor
James M. Wang, Sikorsky Aircraft Corporation; Christopher T. Jones, United Technologies Corporation; Mark. W. Nixon, NASA Langley Research Center

 

A Variational Approach to Multipoint Aerodynamic Optimization of Conventional and Coaxial Helicopter Rotors
Eli Giovanetti and Kenneth Hall, Duke University

 

A Variational Method for Computing the Optimal Aerodynamic Performance of Conventional and Compound Helicopters
Hall, Kenneth; Hall, Steven

 

A Vector Airspeed Measuring System (Vams)* For Helicopters And Other V/Stol Aircraft
E. J. Durbin; G. Born; R. Vause

 

A Versatile Display System for NOE Operations
W.P. Keane, N.K. Shupe, P.B. Sun, T. Robbins, and R. W. Campagna

 

A Versitile Approach to Cockpit Management
Nieuwsma, Harlan J., Cockpit Management Systems; Cramer, Robert L., Rockwell International

 

A Vibration Monitoring Acquisition & Diagnostic System for Helicopter Drive Train Bench Tests
D.A. Dousis. Bell Helicopter Textron Inc.

 

A Vibration Study on a Health Usage and Monitoring System Accelerometer Mount in the Time, Frequency, and Modal Domains
Hochmann, David; Limoge, Ed; Bechhoefer, Eric; Crown, Kris

 

A Vibro-Acoustic Methodology for the Detection and Characterization of Spur Gear Tooth Damage
Hood, Adrian; Samuel, Paul; Pines, Darryll. J.

 

A Virtual Sensor System for Helicopter Usage Monitoring
Ben-Zeev, Oren H.; Haas, David J.; Morales, Miguel A.

 

A Viscous Vortex Particle Model for Rotor Wake and Interference Analysis
He, Chengjian Zhao, Jinggen

 

A VTOL Front Line Delivery System UAV Utilizing Counter-Rotating Mono-Tilt-Rotor Technology
Yassini, Siamak

 

A Wind Tunnel Investigation of a Small-Scale Tiltrotor Model in Descending Flight
Anita I. Abrego, NASA Ames Research Center; Kurtis R. Long, Naval Air Warfare Center

 

A Wind-Tunnel Parametric Investigation of Tiltrotor Whirl-Flutter Stability Boundaries
David J. Piatak, NASA Langley Research Center; Raymond G. Kvaternik, NASA Langley Research Center; Mark W. Nixon, NASA Langley Research Center; Chester W. Langston, NASA Langley Research Center; Jeffrey D. Singleton, NASA Langley Research Center; Richard L. Bennett, Bell Helicopter Textron, Inc.; Ross K. Brown, Bell Helicopter Textron, Inc.

 

A-V-I-A-R-M-F-I-C-S Avionics-Armament-Fire Control System For The Cheyenne Weapon System
Larry S. Klivans; David Baskind

 

A109 Power Evolution Of A Concept
Massimo Mazzoletti, Agusta

 

A160T Hummingbird UAS
M. J Adrianns, David Paul, Ben Ingram and Brad P. Gupta, Boeing Advanced Systems

 

AATD APU Erosion Kit for the AH-64 D Apache Longbow
Kinney, Stephen P.

 

AATD Drive Systems R&D Portfolio
Clay Ames, U.S. Army

 

AATD Rotors Portfolio: Demonstrating High Performance and Durable Rotor Technologies
Louis R. Centolanza, Aviation Applied Technology Directorate (AATD)

 

ABC Development Status and Design Considerations for Navy Missions
D.J. Halley, Sikorsky Aircraft Div., UTC

 

ABC Helicopter Stability, Control and Vibration Evaluation on the Princeton Track
D. Halley, Sikorsky Aircraft Div.

 

Abrasion-Resistant Canopy (ARC) Materials Evaluation Project
Steven D. Webster, Bell Helicopter Textron, Peter G. Dehmer, U.S. Army, Kristen Alexander, U.S. Air Force.

 

Abusive Testing of Turboshaft Engines
Gerhard Sonder, General Electric Co.

 

ACA v. USA: The Case That Defined Harold Pitcairn's Legacy

 

ACAP - An Integrated Approach to Composites Manufacture 413
D. Ruck and J. Goldberg, Sikorsky Aircraft

 

ACAP Crashworthiness Analysis By KRASH
Brian L. Carnell and Mukunda Pramanik, Sikorsky Aircraft

 

Accelerated Insertion Of Materials – Composites
Charles R. Saff, Gail L. Hahn, and Karl M. Nelson, The Boeing Company

 

Accelerating Helicopter Design Through Information Technology
Joseph Goldberg, PhD, Sikorsky Aircraft Corp

 

Accelerometer Control
Bartram Kelley

 

Accuracy Assessment of Regime Recognition Algorithms Using Confusion Matrix
Chang-Hee Hong, Technical Data Analysis, Inc.

 

Accurate Bird Strike Simulation Methodology for BA609 Tiltrotor
Smith, Michael; Tho, Cheng-Ho

 

Accurate Euler Simulation Of Parallel Blade-Vortex Interaction
Lei Tang and James D. Baeder, University of Maryland

 

ACE 3-D Mapping of In-Service Airframe Defects
Lin, Vincent

 

ACE 3-D Mapping of In-Service Airframe Defects
Lin, Vincent

 

Achenbach and the 1874 Tail Rotor Helicopter
Liberatore, E.K.

 

Achieving Excellence in HUMS Design & Implementation
Moreno Saporiti, AgustaWestland

 

Achieving Fail Safe Design in Rotors
W. K. Stratton, D. M. Field, R. H. Finney, Boeing/Vertol

 

Achieving Full Benefits of Intergrated Multiplex in the 1980's
D.B. Kanaly, Harris Corporation

 

Achieving HUMS Benefits in the Military Environment - HUMS Developments on the CH-146 Griffon Fleet
Augustin, Michael J.; Bradley, Scott J.

 

Achieving HUMS Program Financial Benefits - 12 years of day to day HUMS operations on the CH-146 Griffon fleet
Alexandre Heroux-Theriault, Bell Helicopter

 

Achieving Safe and Effective UAV Control for the U.S. Army's Bi-Directional Remote Video Transceiver
Cates, Paul; Ericsson, Lars; Higgins, Raymond; Limbaugh, Douglas

 

Achieving Six-Nine's Reliability Using an Advanced Fatigue Reliability Assessment Model
Adams, David; Zhao, Jack

 

Achieving the Degraded Visual Environment: A Novel Methodology for Handling Qualities Flight Test
Carvil E.T. Chalk, U.S. Army

 

Achieving Usage Based Maintenance with HUMS Regime Recognition
Raymond Beale and Mark Davis, Sikorsky Aircraft Corporation; Paul Swindell, Federal Aviation Administration

 

Acoustic Analysis of Compound Helicopters with Trim Variations
Heather M. Barron and Kenneth Brentner and Joseph Horn and Gurbuz Taha Ozdemir and Adam Thorsen, Pennsylvania State University

Abstract: This study presents a prediction method that analyzes the acoustic radiation of compound helicopters when trim is varied. The goal of this project is to develop a strategy which uses the extra degrees of freedom available in a compound rotorcraft to reduce the noise. Noise radiation is an important factor for both military and civilian rotorcraft. There has been limited research on the specific topic of compound rotorcraft acoustics. A notional vehicle with a main rotor, tail rotor, wing, and auxiliary propeller is used in this investigation. A flight simulation model and noise prediction software are coupled together to calculate all of the results. Predictions indicate that with the addition of degrees of freedom, the noise from a compound helicopter can be vastly changed. For example, reducing rotor advancing-tip Mach number will results in a substantial noise reduction in high-speed flight, this can be useful when finding an optimal-noise flight condition. Results also show that changing the thrust produced from an auxiliary propeller does not have a dramatic effect on the overall sound for the vehicle considered, but can be crucial in changing the performance of the aircraft. Combining both advancing-tip Mach number changes along with thrust changes produced the best low noise results.

 

Acoustic Aspects of Active-Twist Rotor Control
Booth, Earl R., Jr.; Wilbur, Matthew L.

 

Acoustic Assessment of 3 Meter Radius Rotor with Whirl Tower Test and Analysis
Arda YÜCEKAYALI and Erdem AYAN, TAI

 

Acoustic Beamforming for Health Monitoring of Helicopter Transmissions
Hood, Adrian A.; Pines, Darryll

 

Acoustic Characteristics of a Model Isolated Tiltrotor in DNW
Earl R. Booth, Jr., NASA Langley Research Center; Megan McCluer, NASA Ames Research Center; Hormoz Tadghighi, The Boeing Company

 

Acoustic Characteristics Of Advanced Model Rotor Systems
Judith M. Gallman and Sandy R. Liu, US Army Aeroflightdynamics Directorate

 

Acoustic Characteristics Of Advanced Model Rotor Systems
Judith M. Gallman and Sandy R. Liu, US Army Aeroflightdynamics Directorate

 

Acoustic Characteristics Of Advanced Model Rotor Systems
Judith M. Gallman and Sandy R. Liu, U.S. Army

 

Acoustic Characteristics of Tail Rotors and the Effect of Empennage Interactions
E.W. Jacobs, J.M. Fitzgerald and R.K. Shenoy, Sikorsky Aircraft

 

Acoustic Directivity of Maneuvering Helicopters Using Wave Tracing Concepts
Ananthan, Shreyas; Leishman, J. Gordon

 

Acoustic Effects Of Rotor-Wake Interaction During Low-Power Descent
Bruce D. Charles, Bell Helicopter Company

 

Acoustic Emission Detection of Damage Occurring in Dynamically Loaded Fiberglass/Epoxy Laminates
S.D. Lantieri

 

Acoustic Flight Test Results For The Sikorsky S-76 Quiet Tail Rotor At Reduced Tip Speed
Eric W. Jacobs, John Mancini, Joseph A. Visintainer, and Tracy A. Jackson, Sikorsky Aircraft Corporation

 

Acoustic Performance Evaluation of an Advanced UH-1 Helicopter Main Rotor System
D. Hoad & D. Conner, U.S. Army Structures Laboratory

 

Acoustic Phasing and Amplification Effects of Single Rotor Helicopter Blade-Vortex Interactions
Ben Wel-C. Sim, University of Maryland; Fredric H. Schimtz, University of Maryland

 

Acoustic Predictions of Manned and Unmanned Rotorcraft Using the Comprehensive Analytical Rotorcraft Model for Acoustics (CARMA) Code System
D. Douglas Boyd, Jr., Casey L. Burley, and David A. Conner, Langley Research Center

 

Acoustic Predictions Using Measured Pressures From a Model Rotor in the DNW
J.A. Visintainer, Sikorsky Aircraft and C.L. Burley and M.A. Marcolini, NASA Langley Research Center and S.R. Liu, U.S. Army AFDD

 

Acoustic Propagation Using Computational Fluid Dynamics
J.D. Baeder and W.J. McCroskey, U.S. Army Aeroflightdynamics Directorate and G.R. Srinivasan, JAI Associates Inc

 

Acoustic Results From a Full-Scale Wind Tunnel Test Evaluating lndividual Blade Control
Stephen M. Swanson, Sterling Software, Inc.; Stephen A. Jacklin, NASA Ames Research Center; Achim Blaas, ZF Luftfahrttechnik, GmbH; Georg Niesl, Eurocopter Deutschland, GmbH; and Roland Kube, DLR, Institute of Flight Mechanics

 

Acoustic Scattering of Rotorcraft Noise
Brentner, Kenneth; Erwin, James; Lee, Seongkyu

 

Acoustic Shock Waves Generated by a Transonic Helicopter Blade
M.P. Isom, Polytechnic Institute of New York

 

Acoustic Test Techniques Developed for Ground Environment Testing of STOVL Aircraft
David Patience and Robert Burns, BAE Systems

 

Acoustic Vibration Characteristics of High Contact Ratio Planetary Gears
C. Yoerkie and A. Chory, Sikorsky Aircraft Division, United Technologies Corporation

 

Acoustical Analysis of Gear Housing Vibration
A. F. Seybert, T. W. Wu, and X. F. Wu, University of Kentucky; Fred B. Oswald, Lewis Research Center

 

Acoustical Analysis of Gear Housing Vibration
A. F. Seybert, T. W. Wu, and X. F. Wu, University of Kentucky; Fred B. Oswald, Lewis Research Center

 

Acoustical Analysis of Gear Housing Vibration
A.F. Seybert, T.W. Wu, and X.F. Wu, University of Kentucky; Frede B. Oswald, Lewis Research Center

 

Acoustics Of UH-60 Black Hawk With Growth Rotor Blades
O. L. Santa Maria and A. W. Mueller, NASA Langley Research Center; D. A. Conner, U. S. Army

 

ACT Demonstrator/ Flying Helicopter Simulator. A New Demonstrator Test Bed for Flight Control and Cockpit Technologies
Heinz-J?rgen Pausder, DLR; Ulrich Butter, Eurocopter; Volker Gollnick, Wehrtechnische Dienststelle f?r Luftfahrzeuge

 

Active Aerodynamic Load Reduction on a Rotorcraft Fuselage with Rotor Effects - A CFD Validation Effort
Brian Allan, Norman Schaeffler, Luther Jenkins and Chung-Sheng Yao, NASA Langley Research Center; Oliver Wong and Philip Tanner, US Army

 

Active Aerodynamic Load Reduction on a Rotorcraft Fuselage with Rotor Effects - A CFD Validation Effort
Brian G. Allan, Norman W. Schaeffler, Luther N. Jenkins, Chung-Sheng Yao, NASA; Oliver D. Wong, Philip E. Tanner, U.S. Army

 

Active Aeromechanical Stability Augmentation using Fuselage State Feedback
Farhan Gandhi, The Pennsylvania State University; William Weller, United Technologies Research Center

 

Active Blade Flaps - The Needs and Current Capabilities
Francois Toulmay, EUROCOPTER S.A.S., Marignane (France); Valentin Klöppel, EUROCOPTER Deutschland, Ottobrunn (Germany); Francois Lorin, EUROCOPTER S.A.S., Marignane (France); Bernhard Enenkl, EUROCOPTER Deutschland, Ottobrunn (Germany); Jacques Gaffiero, EUROCOPTER S.A.S., La Courneuve (France)

 

Active Cabin Vibration Control for Light Single and Twin Engine Helicopters
Martijn Priems, Stefan Dreher and Falk Hoffmann, Eurocopter Deutschland GmbH and Benjamin Kerdreux and J?r?my Jouve, Eurocopter SAS

 

Active Control of a UAV Helicopter with a Slung Load for Precision Airborne Cargo Delivery
Johnson, Eric; Kang, Keeryun; Ottander, John; Prasad, J. V. R.

 

Active Control Of BVI Induced Vibrations Using A Refined Aerodynamic Model And Experimental Correlation
Marino de Terlizzi, University of California; Peretz P. Friedmann, University of California

 

Active Control of Electrically Controlled Rotor for Both Primary Control and Active Vibration Reduction
Ma Jinchao and Lu yang, Nanjing University of Aeronautics and Astronautics

 

Active Control of Flight Path and Critical Loads in Tilt-Rotor Aircraft
Voskuijl, Mark; Walker, Daniel

 

Active Control of Gust- and Interference-Induced Vibration of Tilt-Rotor Aircraft
N.D. Ham, N.M. Wereley, and K.D. von Ellenrieder, Massachusetts Institute of Technology

 

Active Control of Helicopter Transmission Noise
R.H. Spencer, M.J. Burke, G.W. Tye, Boeing Helicopters

 

Active Control of Helicopter Transmission Noise
R.H. Spencer, M.J. Burke, G.W. Tye, Boeing Helicopters

 

Active Control of Helicopter Transmission Noise
R.H. Spencer, Boeing Helicopters; M.J. Burke and G.W. Tye, Noise Cancellation Technologies, Inc.

 

Active Control Of Interior Noise In A Large Scale Cylinder Using Piezoelectric Actuators
H. C. Lester and R. J. Silcox, NASA Langley Research Center

 

Active Control Of Interior Noise In A Large Scale Cylinder Using Piezoelectric Actuators
H. C. Lester and R. J. Silcox, NASA Langley Research Center

 

Active Control Of Interior Noise In A Large Scale Cylinder Using Piezoelectric Actuators
H.C. Lester and R.J. Silcox, NASA Langley Research Center

 

Active Control of The Helicopter Rotor for Vibration Reduction
J. Shaw And N. Albion, Boeing Vertol Co.

 

Active Control of Transmission Noise in a Bell 407 Helicopter
Anant Grewal, CNRC; Sébastien Laurier Chapleau, BELL Helicopter Textron; Yann Pasco and Alain Berry, Université de Sherbrooke

 

Active Control System for Helicopter Vibration Reduction By Higher Harmonic Pitch
R.B. Taylor & F.A. Farrar, United Technologies Research Center & W. Miao, Sikorsky Aircraft Div., UTC

 

Active Control Technology to Improve Mission Effectiveness
Philippe Rollet, Eurocopter; Serge Mezan, Eurocopter

 

Active Control Technology to Improve Mission Effectiveness
Philippe Rollet, Eurocopter; Serge Mezan, Eurocopter

 

Active Controller for Comanche Air Resonance Stability Augmentation
Blackwell, Robert; Kothmann, Bruce; Mychalowycz, Evhen; Panda, Brahmananda

 

Active Controller Performance Requirements
Einthoven, Pieter

 

Active Crash Protection System Enhancements
A. Bolukbasi, T. Birchette, J. Schaub, M. Moody, and R. Fisher, The Boeing Company; L.A. Powell, Y.-T. Choi, W. Hu, and N.M. Wereley, University of Maryland; J. Woodhouse, U.S. Army

 

Active Crash Protection Systems for UAVs
Bolukbasi, Akif

 

Active Elimination of Stall Conditions
M. Kretz, Giravions Dorand Industries

 

Active Flap Control for Vibration Reduction and Performance Improvement
F. K. Straub, McDonnell Douglas Helicopter Systems

 

Active Flap System for an Advanced CH-47 Rotor
Friedrich Straub and Edward Brouwers and Richard Bussom, Boeing, Louis Centolanza, US Army, AATD, Terry Birchette, The Boeing Company

 

Active Flaps and Slats for Rotor Performance Enhancement
Kumar Ravichandran, University of Maryland; Inderjit Chopra, University of Maryland; Brian Wake, United Technologies Research Center; Benjamin Hein, Sikorsky Aircraft Corp

 

Active Flaps for Noise Reduction: A Computational Study
Patt, Dan; Liu, Li; Friedmann, Peretz P.

 

Active Flight Control and Applique Inceptor Concepts for Autorotation Performance Enhancement
Jeffrey Keller, Continuum Dynamics, Inc.; Robert McKillip, Continuum Dynamics, Inc.; Joseph Horn, Pennsylvania State University; Thanan Yomchinda, Pennsylvania State University

 

Active Flow Control Measurements and CFD on a Transport Helicopter Fuselage
Martin, P. B.; Tung, C.; Hassan, Ahmed A.; Cerchie, D.; Roth, J.

 

Active Flow Control on Separation and Post-Stall of Rotor Airfoil by Using Synthetic Jet and Parametric Analyses
Zhao Guo-Qing, Zhao Qi-Jun, Nanjing University of Aeronautics and Astronautics

 

Active Interrogation Of Helicopter Rotor Faults Using Trailing Edge Flap Actuation
Patricia W. Stevens, The Pennsylvania State University; Edward C. Smith, The Pennsylvania State University

 

Active Man-Machine Interface for Advanced Rotorcraft
Allen L. Zaklad, Monica Z. Weiland, Wayne W. Zachary, Clarence A. Fry, CHI Systems Inc.; James W. Voorhees, Advanced Simulation Engineering

 

Active Parallel Actuation Subsystem, An Alternative Approach to Tactile Cueing Without Fly By Wire
Adam Taylor, BAE Systems; Joe Irwin, The Boeing Company

 

Active Pitch Link Actuator for Impedance Control of Helicopter Vibration
Feszty, Daniel; Mander, Andrei; Nitzsche, Fred

 

Active Rotor Control (ARC) of a Mach-Scale Trailing Edge Flap Rotor
A.P.F. Bernhard, Sikorsky Aircraft Corporation; J. O?Neill, Sikorsky Aircraft Corporation; F. Kohlhepp, Sikorsky Aircraft Corporation; W. Welsh, Sikorsky Aircraft Corporation; P. Lorber, United Technologies Research Center

 

Active Rotor Controls for Vibration Reduction and Performance Enhancement
Kumar Ravichandran, Shreyas Ananthan, Inderjit Chopra, University of Maryland; Benjamin Hein, Sikorsky Aircraft

 

Active Rotor Experiments at Mach Scale Using Root Pitch IBC
Peter Lorber, United Technologies Research Center; Christopher Park, United Technologies Research Center; David Polak, United Technologies Research Center; John O?Neill, Sikorsky Aircraft Corporation; William Welsh, Sikorsky Aircraft Corporation

 

Active Structural Acoustic Control of a Bell 407 Transmission Noise
P. Belanger, A. Berry, Y. Pasco, Universit? de Sherbrooke; Y. St-Amant, Universit? Laval; S. Rajan, Bell Helicopter Textron

 

Active Trim Tab for Rotor Track and Balance
Attila Lengyel and Dr. Marthinus van Schoor, Midé Technology Corporation; Dr. Louis Centolanza, U.S. Army

 

Active Vibration and Noise Reduction in Rotorcraft Using Aeroelastic Simulation
P. Friedmann, L. Liu, D. Patt, Univ. of Michigan

 

Active Vibration Control Actuation
Christopher D. Lesser and Darvin D. Remington, Moog Inc.

 

Active Vibration Control of Rotorcraft Driveshaft-Airframe Dynamics
Hans A. DeSmidt, The Pennsylvania State University; K. W. Wang, The Pennsylvania State University; E. C. Smith, The Pennsylvania State University

 

Active Vibration Control Strategy For Tiltrotor Aircraft
Mark A. Norris, Andrew D. Meyers, Todd R. Haughee, Lord Corporation

 

Active Vibration Control Using Fluidlastic Pylon Struts
D.P. McGuire, Lord Corporation

 

Active Vibration Suppression for the CH-47D
R. S. Teal, D. L. McCorvey, and D. Malloy, Boeing Defense & Space Group, Helicopter Div.

 

Active Vibration Treatment for Rotorcraft with Piezo-Live Technology
Michael R. Smith, Taeoh Lee, Donald J. Merkley

 

Active-Passive Hybrid Optimization of Rotor Blades with Trailing Edge Flaps
Jianhua Zhang, The Pennsylvania State University; Edward C. Smith, The Pennsylvania State University; K. W. Wang, The Pennsylvania State University

 

Active-Twist Rotor Control Applications For UAVs
Matthew L. Wilbur and W. Keats Wilkie, U.S. Army

 

Active/Passive Aircraft Survivability (APAS) Program
Clifford, Jerome

 

Active/Passive Vibration Reduction and Performance Enhancement of Helicopter Rotors at High Advance Ratios
Friedmann, Peretz Glaz, Bryan; Liu, Li

 

Actuation Requirements of Swashplateless Trailing-Edge Flap Helicopter Rotor in Maneuvering and Autorotation Flights
Chopra, Inderjit; Shen, Jinwei

 

Actuator and Hydraulic Survivability Concepts for Hughes YAH-64
Ray A. York, Ralph E. Molloy, Eric G. Adler, Bertea Corporation

 

ADAMS Modeling of a Helicopter on a Ship which Undergoes Roll, Pitch, Heave and Sway
Richard Weisenburger and Brian Hamilton, The Boeing Company

 

Adaptable Gas Turbine Blade Concept Study
Muthuvel Murugan, David Booth and Anindya Ghoshal and Douglas Thurman and  Kevin Kerner, US Army

 

Adaptation of a Ground Proximity Warning System for Rotorcraft
Maj Doug Schueler, Naval Air Warfare Center; Mr. John Durkin, Cubic Defense Systems; Rick Funchion, Naval Air Warfare Center

 

Adaptation Of A Modern Medium Helicopter (Sikorsky S-76) To Higher Harmonic Control
James J. O'Leary, Dr. Sesi B.R. Kottapalli, United Technologies Corporation; Mark Davis, United Technologies Research Center

 

Adaptation of Pultrusion to the Manufacture of Helicopter Components
E. Blake, Bell Helicopter Textron and N. Tessier, AMMRC

 

Adaptation of Pultrusion to the Manufacture of Helicopter Components
E. Blake, Bell Helicopter Textron and N. Tessier, AMMRC

 

Adapting a Small Ground Turbine to Very Light Airborne Applications: a "Lean" Approach
Gasparini, Giuseppe; Gasparotto, Giovanni; Piazzoli, Mauro; Rossi, Teddi

 

Adapting Air to Ground Acquisition Systems to the Air to Air Task
E. Wilson, McDonnell Douglas Helicopter Co.

 

Adapting and Expanding Rotorcraft Decision Aids for the Battle Commander
Janice Hess, Lockheed Martin Systems Integration; Stephen Patteson, Lockheed Martin Systems Integration

 

Adaptive Algorithms for Rotorcraft Active Vibration Control
Heverly, David; Pappas, John; Singh, Rupinder

 

Adaptive Distributed Aviation Asset Optimization for Operational Effectiveness
Charles Shepard, Bell Helicopter, John Merrihew, VELOXITY, Larry Lafferty, VELOXITI

 

Adaptive Distributed Aviation Asset Optimization for Operational Effectiveness
Charles Shepard, Bell Helicopter, John Merrihew, VELOXITY, Larry Lafferty, VELOXITI

 

Adaptive Distributed Aviation Asset Optimization for Operational Effectiveness (Phase II)
Charles Shepard and John Merrihew and Norm Geddes and Steve Toney and Larry Lafferty, VELOXITI, Inc.

 

Adaptive Electronic Fuel Control Test Techniques
C.E. Greenberg, Sikorsky Aircraft Division, UTC

 

Adaptive Fuel Control Feasibility Investigation
R.L. Bolton, U.S. Army Research and Technology Laboratories

 

Adaptive Fuel Control Testing
D.M. Achgill, Allison Gas Turbine Division, General Motors Corp. and R.D. Zagranski, Chandler Evans Control Systems Division, Colt Industries

 

Adaptive Grid Sequencing and Interpolation Schemes for Accelerated Rotor Free-Wake Analyses
Ashish Bagai and J. Gordon Leishman, University of Maryland

 

Adaptive Guidance and Control for Autonomous Formation Flight

Jongki Moon, Ramachandra Sattigeri, J.V.R. Prasad, Anthony J. Calise, Georgia Institute of Technology

 

Adaptive Limit and Control Margin Prediction and Limit Avoidance
Yavrucuk, Ilkay; Prasad, J. V. R.; Calise, Anthony J.; Unnikrishnan, Suraj

 

Adaptive Limit Margin Prediction and Control Cueing for Carefree Maneuvering of VTOL Aircraft
Ilkay Yavrucuk, J.V.R. Prasad, Georgia Institute of Technology

 

Adaptive Magnetorheological Landing Gear Dampers Employing Passive Valves to Maximize Applicable Sink Rate Range
Akif O. Bolukbasi and Terrence S. Birchette, The Boeing Company, JIn Woodhouse, Aviation Applied Technology Directorate, Norman Wereley and Louise A. Powell and Young-Tai Choi and Wei "Peter" Hu, University of Maryland

 

Adaptive Magnetorheological Snubber Lag Damper (MRSLD) for Hingeless Helicopter Main Rotor Blades
Hu, Wei; Kothera, Curt; Ngatu, Grum; wereley, Norman

 

Adaptive Model Inversion Flight Control For Tiltrotor Aircraft
Rolf T. Rysdyk, Georgia Institute of Technology; Anthony J. Calise, Georgia Institute of Technology

 

Adaptive Path Planning in a Dynamic Environment using a Receding Horizon Probabilistic Roadmap: Experimental Demonstration
Thomas A. Frewen, Harshad Sane, United Technologies Research Center; Marin Kobilarov, California Institute of Technology; Sanjay Bajekal, Konda R. Chevva; United Technologies Research Center

 

Adaptive Thermodynamic Engine Model for the Next Generation Control Systems for Helicopter Engines
Desai, mihir C.; Crainic, Cristina

 

Adaptive Vehicle Management Systems Phase I Overview
Russell Enns and George Lukes and James Dryfoos and Bryan Kashawlic and Pam Hayes, The Boeing Company

 

Adaptive Workspace - A Technical Solution for Managing Aviation Operations
Samad Muhammad, Atlantic Software Technologies, Inc. and Joel Statkevicus, Sikorsky Aircraft Corporation

 

Addendum to 10th Annual Forum -- Theory of Rotor Blade Uncoupled Lag Bending Aero-Elastic Vibrations
Peter F. Leone, Kellett Aircraft Corporation

 

Adding Realism to Inverse Simulation of Helicopters in Aggressive Maneuvering Flight Using a Receding Horizon Approach
Anderson, David; Bagiev, Marat; Murray-Smith, David; Thomson, Douglas

 

Additive Manufacturing & Sustainability An OEM’s Perspective
Kathleen Oldham, Bell Helicopter Textron Inc.

 

Additive Manufacturing & Sustainability An OEM’s Perspective
Kathleen Oldham, Bell Helicopter Textron Inc.

 

Additive Manufacturing And Sustainability
François Richard, Pratt & Whitney

 

Additive Manufacturing And Sustainability
François Richard, Pratt & Whitney

 

Additive Manufacturing For Propulsion
Brian Hann, Honeywell

 

Additive Manufacturing for the Aerospace Industry
Darin Thomas and Greg Sabin, Southeastern Tool and Die

 

Additive Manufacturing of Ti-6Al/4V Firewalls
Hal Brody and Rainer Hebert, University of Connecticut, Michael Urban and William Harris, Sikorsky Aircraft, Salay Stannard, JTI Inc

 

Addras - An Integrated Systems Approach
Lawrence E. Becker and Charles K. Rutledge, Lockheed Engineering and Sciences Company; Robert E. Grandle and Robert A. Golub, NASA; Rita A. Smith, Lockheed Engineering and Sciences Company

 

Addras - An Integrated Systems Approach
Lawrence E. Becker and Charles K. Rutledge, Lockheed Engineering and Sciences Company; Robert E. Grandle and Robert A. Golub, NASA; Rita A. Smith, Lockheed Engineering and Sciences Company

 

ADDRAS - An Integrated Systems Approach
Lawrence E. Becker and Charles K. Rutledge, Lockheed Engineering and Sciences Company; Robert E. Grandle and Robert A. Golub, NASA/LAC/AcoD; Rita A. Smith, Lockheed Engineering and Sciences Company

 

Addressing the Challenges Facing the Rotorcraft Industry
Marc Paganini, American Eurocopter

 

Addressing Today’s Aeromechanic Questions by Industrial Answers
M. Dietz, C. Maucher, D. Schimke, Eurocopter Deutschland GmbH

 

Adjoint-Based Design of Rotors Using the Navier-Stokes Equations in a Noninertial Reference Frame
Jones, William; Lee-Rausch, Elizabeth; Nielsen, Eric

 

Adjoint-Based Unsteady Airfoil Design Optimization with Application to Dynamic Stall
Karthik Mani, Brian Lockwood and Dimitri Mavriplis, University of Wyoming

 

ADS 33 Handling Qualities Evaluation of Advanced Response Types Control Laws on the ACT/FHS Demonstrator
Brisset, Nicolas; M?zan, Serge

 

ADS-33 Evaluation of the International CH-47 Chinook
Christopher Colosi, Pieter Einthoven and Erik Kocher, The Boeing Company; Matthew Parsons and Bryan Carrothers, Canadian Department of National Defence

 

ADS-33 Handling Qualities Evaluation of the UH-60M Fly-By-Wire Demonstration Aircraft
Frank Luria and F. Scott Smith, US Army AED (AMRDEC); Jeffrey Harding, Harding Consulting, Inc. and Adam Mouser, US Army Aviation Flight Test Directorate

 

ADS-33C Flight Test Maneuvers Validation in a Degraded Visual Environment
Daniel C. Hart, US Army Aeroflightdynamics Directorate

 

ADS-33E Maximum Takeoff Gross Weight Handling Qualities Of The H-60 Helicopter
David E. Bischoff, Michael P. Fallon, David D. Kyser, Naval Air Systems Command

 

ADS-33E Predicted and Assigned Low-Speed Handling Qualities of the CH-47F with Digital AFCS
Blanken, C. L.; Einthoven, Pieter; Irwin, Joseph; Miller, David

 

ADS-33E-PRF Specification Application Package (ASAP)
Roger Hoh and Thomas Nicoll, Hoh Aeronautics; Robert Heffley, Robert Heffley Engineering and David Mitchell, Mitchell Aerospace Research

 

ADS-89-SP: A Standard Practice for U.S. Army Rotorcraft Structural Integrity Program
Michael R. Kiser, Kristina N. Marshall, US Army

 

Advance Technology Impacts on Rotorcraft Weight
E. Vega, Hughes Helicopters, Inc

 

Advanced Adaptive Model-Based Engine Control, Engine Test Results
Desai, Mihir; Koziol, Paul Mattice, Jeff; Smith, Bert; Storey, Bill

 

Advanced Aeroelastic Optimization Applied to an Improved Performance, Low Vibration Rotor
Frank Tarzanin, The Boeing Company; Darrell K. Young, The Boeing Company; Brahmananda Panda, The Boeing Company

 

Advanced Affordable Turbine Engine (AATE)
Anastasia Kozup, U.S. Army

 

Advanced Aircraft Electrical System And Its Application To Helicopters
A. J. Marek; J. R. Perkins

 

Advanced Aluminum Alloys for Improved Rotorcraft Reliability
Gerard J. Nanni, Bell Helicopter Textron, Inc.

 

Advanced Apache Drive System
Thomas L. Doubts, Boeing

 

Advanced Approaches to Helicopter Engine System Dynamics
Eric Ho, Pratt & Whitney Canada

 

Advanced Attack Helicopter Fatigue Testing: Overview
George D. Deveaux, Hughes Helicopters

 

Advanced Attack Helicopter Fatigue Testing: Overview
George D. Deveaux, Hughes Helicopters

 

Advanced Attitude Command Generation for a Helicopter UAV in the Context of a Feedback Free Reference System
Johann C. Dauer, Sven Lorenz, and Joerg S. Dittrich, German Aerospace Center

 

Advanced Beam Modeling Applied to Articulated Rotor - Implementation in HOST Aeromechanic Simulation Tool
Yan Skladanek and Laurent Boucherie and Bernard Benoit and Paul Cranga, Airbus Helicopters

 

Advanced Black Hawk Drive System Technology
Bruce Hansen, Sikorsky Aircraft

 

Advanced Cargo Aircraft Size Optimization
C.P. Van Buiten, Sikorsky Aircraft Div., UTC

 

Advanced CBM Technologies for Helicopter Rotor Systems - Full Scale Rotor Demonstration and Test Results
Andrews, James; Augustin, Michael

 

Advanced CFD-based Optimization Methods Applied to the Industrial Design Process of Airframe Components at Airbus Helicopters
Qinyin Zhang and Andrea Garavello and Alessandro D'Alascio and Dieter Schimke, Eurocopter Germany

 

Advanced Civil Tiltrotor Design Optimization and Issues
David R. Schleicher, NASA Ames Research Center

 

Advanced Cladding for Helicopter Rotors
D.P. Huey and A.R. Stetson

 

Advanced Composite Airframe Program (ACAP) Preliminary Design
L.T. Mazza, USA RTL Applied Technology Lab & Dr. R. L. Foye, USA RTL Aero Lab

 

Advanced Composite Helicopter Misers Gold Test/Analysis
Mary Ann Partridge, Michael L. Atkinson, Lawrence J. Mente, Kaman Sciences Corporation; Kellie B. Unsworth, U.S. Army

 

Advanced Composite Main Rotor Flexbeam from Optimization to Full Scale Multicomponent and Whirl Tower Testing
B.K. Hamilton; N.W. Bell; R.J. Murrill; S.E. Flores; L.A. Lucchetto, McDonnell Douglas Helicopter Company

 

Advanced Composites - Designed to Survive
Nikolaos Caravasos, J. Patrick Donnelly, Boeing Vertol Company

 

Advanced Computerised Support Systems For The Apache and Chinook Helicopters
Alan Cort, Aerosystems International

 

Advanced Design Infra-Red Suppressors for Turboshaft Engines
W.H. Barlow and A. Petach

 

Advanced Development Project Office: Naval UAV And UCAV Brief
CDR Osa Fitch, USN; Clint Housh and Marcie Langelier

 

Advanced Dynamic Simulation for Determination of Landing Gear Loads
Nicholas, Joe

 

Advanced Engine Controls and Accessories for Helicopter Applications
Roger Furgurson, USAAMRDL Eustis Directorate

 

Advanced Engine Controls and Accessories for Helicopter Applications
Roger Furgurson, USAAMRDL Eustis Directorate

 

Advanced Flight Control Development for Single-Pilot Attack Helicopters
R. Hendrick, G. Ramohalli and D. Yanke, Honeywell, Inc. and R. Fortenbaugh and T. Freeman, Bell Helicopter Textron, Inc

 

Advanced FTIR Spectral Measurements of Low Contrast Rotorcraft Targets
Shepherd, Robert A.

 

Advanced Fuel Control System for Turboshaft Engines
C. Orkin and G. Haliscak, Kaman Aerospace Corp.

 

Advanced Gear Alloys for Ultra High Strength Applications
Jason Sebastian, QuesTek Innovations LLC; Timothy Krantz, NASA Glenn Reseach Center; Tony Shen, The Boeing Company

 

Advanced Genetic Algorithms for Designing Complex Laminated Composite Structures
Grant Soremekun, ADOPTECH, Inc.; Zafer Gürdal, Virginia Tech

 

Advanced Helicopter Avionics
A. Raz, Elbit Computers Ltd.

 

Advanced Helicopter Pilotage Visual Requirements
J.S. Seeman, J. DeMaio, S. Justice, and J. Wasson, McDonnell Douglas Helicopter Co.; P. Derenski, M. Hunter, and L. Walrath, McDonnell Aircraft Co.

 

Advanced HUMS And Vehicle Management Systems Implemented Through An IMA Architecture
Ronald M Stewart, Piet Ephraim, Stewart Hughes Limited

 

Advanced Ice Protection Systems Test in the NASA Lewis Icing Research Tunnel
Thomas H. Bond and Jaiwan Shin, NASA Lewis Research Center and Geert A. Mesander, USAF

 

Advanced IPS Technology Enabling Advanced VLA Design
Philip H. Snyder, Rolls-Royce North American Technologies, Inc.

 

Advanced IR Suppression Technology
Mac Dinning, AATD

 

Advanced Light Emitting Diode (LED) Displays-Paced By Technology Or Systems Application?
J. Wright, Litton Systems Canada

 

Advanced Lube System Diagnostics for V-22
H.M. Belman and F. DiPasquale, TEDECO Division, Aeroquip Corp.

 

Advanced Machining Techniques On Titanium Rotor Parts
Edmund P. Leigh, Bell Helicopter Textron, Inc.; John K. Schueller, University of Florida; Scott Smith, University of North Carolina; Jiri Tlusty, University of Florida

 

Advanced Methodology for Quality Control of Composite Rotor Blades at Bell Helicopter Textron
B. Rupe and B.J. Hunter, Bell Helicopter Textron

 

Advanced Methods of Helicopter Propulsion System Integration/Air Management System Design
K.E. Boyd and E. Murgia, McDonnell Douglas Helicopter Co.

 

Advanced Mobile Flight Control Development and Deployment Center
Willard J. Harris, The Boeing Co.; John Krainski, The Boeing Co.

 

Advanced Modeling and Flight Control Design for Gust Alleviation on Ship-Based Helicopters
Bridges, Derek; Geiger, Derek; Horn, Joseph; Polsky, Susan; Sahasrabudhe, Vineet

 

Advanced Models for Helicopter Gearbox Health Management
Robert G. Tryon, Richard Holmes, Raja V. Pulikollu, VEXTEC Corporation

 

Advanced Multi Axis Trim and Drill Cell for Low Volume, Multiple Part Configuration in a JIT Environment
Andrew Laird, Bell Helicopter Textron Canada

 

Advanced Rain And Sand Erosion Resistant Elastomers
Shek C. Hong, Hontek Corporation; Tommy J. Wiggins, U.S. Army Aviation and Missile Command

 

Advanced Reconfigurable Communications, Fault Tolerant Avionics
Barrera, Ralph E.; Langley, Richard

 

Advanced Rotary-Wing Handling Qualities
Major Paul R. Curry and Mr. James T. Matthews, Jr., USATRECOM

 

Advanced Rotor Aerodynamics Concepts with Application to Large Rotorcraft
Matthew W. Floros, Raytheon ITSS; Wayne Johnson, Army/NASA Rotorcraft Division; Michael P. Scully, Aeroflightdynamics Directorate (AMRDEC)

 

Advanced Rotor Computations with a Corrected Potential Method
J.O. Bridgeman, Woodside Summit Group, R.C. Strawn and F.X. Caradonna, U.S. Army Aeroflightdynamics Dir., and C.S. Chen, National Research Council

 

Advanced Rotor Wake Interference Modeling for Multiple Aircraft Shipboard Landing Simulation
He, Chengjian; Xin, Hong; Bhagwat, Mahendra

 

Advanced Rotorcraft Design for Future Civil Operations
Michel Polychroniadis, Eurocopter

 

Advanced Rotorcraft Transmission Development-A Technology Reconversion Program
Y. D. Chen, G. Heath, R. Gilbert, and V Sheth, McDonnell Douglas Helicopter Systems

 

Advanced Rotorcraft Transmission II - Demonstrator Design
Eric C. Ames, Fort Eustis; Zachary S. Henry, Bell Helicopter Textron Incorporated

 

Advanced Rotorcraft Transmission Program
R.C. Bill, Propulsion Directorate, U.S. Army AVSCOM

 

Advanced Rotorcraft V/STOL-Rotary Wing with Airplane Qualities
J.J. Schneider and J.B. Wilkerson, Boeing Helicopters

 

Advanced Scout Helicopter Flying Qualities Requirements--How Realistic Are They?

D.M. Pitt & F.E. Heacock, US Army AVRADCOM

 

Advanced Simulation and Control of Engine Inlet Distortion Using Virginia Tech StreamVane Technology
Walter F. O’Brien, K. Todd Lowe, Virginia Tech

 

Advanced Structural Casting Applications for a Gas Turbine Engine
E.F. Bishop, J.N. Fleck and T.M. Regan, General Electric Co

 

Advanced Structural Joint Concepts
May, Carl; Wilson, Henry; Hethcock, J. Donn; Davis, Tim

 

Advanced Structures Concepts R&M/Cost Assessments
T.N. Cook, Sikorsky Aircraft Div., UTC & T.E. Condon, USA RTL Applied Technology Lab

 

Advanced Subsystems Status Monitor
J.P. McGee, Sikorsky Aircraft Div., UTC

 

Advanced Surface Hardening Technologies
M.S. Chatterjee, Allison Gas Turbine Division, GM Corporation

 

Advanced System And Technology Integration: Airborne Application
L. B. Giles, Bell Helicopter Textron, Inc.; E. C. Vaught, Bell Helicopter Textron, Inc.

 

Advanced System And Technology Integration: The Supercockpit
C. D. Holley, Bell Helicopter Textron, Inc.

 

Advanced System And Technology Integration: The Supercockpit
C. D. Holley, Bell Helicopter Textron, Inc.

 

Advanced Systems Applications - Foundations for LHX
R.E. Parks & T.W. Ingram, Bell Helicopter Textron

 

Advanced Tactical Combat Model (ATCOM) Team Behavior Modeling of the Apache Longbow
Bill Baker, The Boeing Company

 

Advanced Technologies Applied To PT6C-67A Tiltrotor Engine Design
H. Smailys, Pratt & Whitney Canada; M. Chabot, Pratt & Whitney Canada; J. Chamoun, Pratt & Whitney Canada; D. Chmiel, Pratt & Whitney Canada; D. Jermyn, Pratt & Whitney Canada; S. Kacker, Pratt & Whitney Canada; F. Lefebvre, Pratt & Whitney Canada; C. Litalien, Pratt & Whitney Canada; K. Patel, Pratt & Whitney Canada; P. Stuttaford, Pratt & Whitney Canada

 

Advanced Technologies Applied To PT6C-67A Tiltrotor Engine Design
H. Smailys, M. Chabot, J. Chamoun, D. Chmiel, D. Jermyn, S. Kacker, F. Lefebvre, C. Litalien, K. Patel, and P. Stuttaford, Pratt & Whitney Canada

 

Advanced Technologies as Applied to the Design of the HLH Rotor Hub
H. K. Reddick, Jr., USAAMR&DL, Eustis; C. D. McCall, and D. M. Field, Boeing Vertol

 

Advanced Technologies for Application to the Rotorcraft Technical Architecture
Jay Pruiett, Smiths Aerospace; Tim Skutt, Smiths Aerospace

 

Advanced Technologies for High Performance NH90 Blades
Claude, Quillien; Rauch, Patrice

 

Advanced Technologies for Rotor System CBM
Augustin, Michael; Yeary, David

 

Advanced Technology Blade Testing on the XV-15 Tilt Rotor Research Aircraft
Brent Wellman, NASA Ames Research Center

This paper was not submitted in time to be included in the printed Proceedings.

 

Advanced Technology Cockpit Simulator
Alan H. Shaw, Westland Helicopters Ltd

 

Advanced Technology Helicopter Landing Gear
William T. Alexander, Jr., U.S. Army; Ralph E. Goodall, Hughes Helicopters

 

Advanced Technology Impact on LHX Helicopter Preliminary Design
J.P. Rogers, R.A. Shinn and R.L. Smith, U.S. Army Aviation Systems Command

 

Advanced Technology To Meet Helicopter Market Requirements
A. CASSIER, EUROCOPTER

 

Advanced Technology Transition and the CT7-5 Technology Demonstrator Engine
Coleman, Michael; Kingery, John; Kirtley, Kevin; Spring, Samuel

 

Advanced Transmission Component Development
K. Rosen & H. Frint, Sikorsky Aircraft Division, UTC

 

Advanced Transmission Studies
Dr. J.J. Coy, NASA Lewis Research Center and Dr. R.C. Bill, U.S. Army Propulsion Directorate

 

Advanced Turbine Engines - An Air Force Vision
Richard Hill, USAF

 

Advanced Vertical Lift Configuration Study
Foster, Malcolm

 

Advanced Workload Assessment Techniques for Engineering Flight Simulation
J.F. Grenell, Boeing Defense & Space Group and A.F. Kramer, E.J. Sirevaag and C.D. Wickens, University of Illinois

 

Advanced-Composite Joints and Fittings for Primary Structural Components
Harminder S. Saluja, Boeing Vertol Company

 

Advancements in Dimensional Inspection of Helicopter Gearbox and Transmission Cases
E.V. Maier, Bell Helicopter Textron

 

Advancements in Erosion Testing of Rotor Blade Leading Edges
D.A. Haynie, Bell Helicopter Textron

 

Advancements in I.R. Suppressors for Helicopters
Clifford Banthin, AVCO Lycoming

 

Advancements Toward Oil-Free Rotorcraft Propulsion
Bruckner, Robert; Howard, Samuel; Radil, Kevin

 

Advances And Applications Of Pyrowear 53 In Helicopter Transmission Systems
Robert DiRusso, Kaman Aerospace Corporation

 

Advances In Decelerating Steep Approach And Landing For Helicopter Instrument Approaches

P.S. Demko, J.H. Boschma, US Army Avionics R & D Activity

 

Advances in Full Rotorcraft Simulations with Unstructured CFD
Abras, Jennifer; Lynch, C.; Smith, Marilyn

 

Advances in Rotorcraft Integrated Avionics
Redman, David A.

 

Advances in the Understanding of Autogyro Flight Dynamics
Houston, Stewart; Thomson, Douglas

 

Advancing Blade Concept (ABC Tm) Development
Andrew J. Ruddell

 

Advancing Blade Concept (ABC) TM Dynamics
J. T. L. Abbe, R. H. Blackwell, and D. S. Jenney

 

Advancing Blade Concepts (ABC TM) High Speed Development
A.J. Ruddell, Sikorsky Aircraft Div., UTC & J.A. Macrino, USA TRL Applied Technology

 

Advancing Tiltrotor State-of-the-Art With Variable Diameter Rotors
E.A. Fradenburgh and D.G. Matuska, Sikorksy Aircraft Div., UTC

 

Advantages of Centrifugal Compressors in Helicopter Gas-Turbine Engines
S. D. Hage

 

Advantages Of Vectored Thrust For Joint Heavy Lift
Anthony A. duPont, duPont Aerospace Company, Inc.

 

Advantages of Vectored Thrust for Joint Heavy Lift
Dupont Aerospace Company, Inc.

 

Adverse Effects Of Downwash Upon Man
William P. Schane, M.D., LTC, MC, F/S, U.S. Army

 

Adverse Environment Rotor Test Stand Calibration Procedures and Ice Shape Correlation
Brouwers, Edward; Han, Yiqiang; Palacios, Jose; Smith, Edward

 

Adverse Environment Rotor Test Stand Calibration, Ice Adhesion and Ultrasonic De- Icing Testing
Dr. Jose Palacios, Pennsylvania State University

 

AE 1107 (T406) Engine Growth Paths And Methodologies
Emanuel Papandreas, Roll-Royce

 

AE 1107 Engine Growth Paths and Methodologies
John G. Nourse, Rolls-Royce

 

AEFA/Boeing Demonstration of the Effectivity of the YUH-61A in Moderate Icing Conditions
MAJ J.F. Hagen, D.V. Lewis, and J.S. Reid

 

Aerial Application and the Rise of American Rotorcraft
Connor, Roger

 

Aerial Jeep Retrospective
Piper, Robert R.

 

Aeroacoustic Flight Test and Data Analysis for the Validation of Fenestron Noise Computations
F. Falissard, F. Desmerger, P. Gardarein, L. Binet, ONERA; J.-C. Camus, DGA Flight Test

 

Aeroacoustic Flowfield and Acoustics of a Model Helicopter Tail Rotor at High Advance Ratio
R.K. Shenoy, Sikorsky Aircraft Division, UTC

 

Aeroacoustic Prediction Tools For Quiet Rotor Design And Optimization At ONERA
Y. Delrieux, J. Prieur and D. Declerck, Office National d'Etudes et de Recherches Aérospatiales

 

Aeroacoustic Simulation of an EC145-T2 Rotor in Descent Flight
Sascha Schneider, Airbus Helicopters Deutschland GmbH; Ulrich Kowarsch and Daniel Lippert and Manuel Keáler and Ewald Kr„mer, University of Stuttgart

 

Aeroacoustic Simulation of an EC145-T2 Rotor in Descent Flight
Ulrich Kowarsch, Daniel Lippert, University of Stuttgart; Sascha Schneider, Airbus Helicopters Deutschland GmbH; Manuel Keßler and Ewald Krämer, University of Stuttgart

 

Aeroacoustics of a Coaxial Rotor in Level Flight
Brown, Richard; Duraisamy, Karthikeyan; Kim, Hyo Won

 

Aerobatic Planforms for Hovering MAVs
Richard Ames, Oliver Wong, and Narayanan Komerath, Georgia Institute of Technology

 

Aerobots as a Ubiquitous Part of Society
Larry A. Young, NASA

 

Aerodynamic Analysis And Measurement Of A Subwing Blade Tip Shape For Blade-Vortex Interaction Noise Reduction
Albert G. Brand, Bell Helicopter Textron, Inc.

 

Aerodynamic And Acoustic Calculations Of Transonic Nonlifting Hovering Rotors
J. Prieur and M. Costes, ONERA; J. D. Baeder, NASA Ames Research Center

 

Aerodynamic And Acoustic Calculations Of Transonic Nonlifting Hovering Rotors
J. Prieur and M. Costes, ONERA; J. D. Baeder, NASA Ames Research Center

 

Aerodynamic And Acoustic Calculations Of Transonic Nonlifting Hovering Rotors
J. Prieur and M. Costes, ONERA; J.D. Baeder, U.S. Army

 

Aerodynamic and Acoustic Design of a Low Noise Dual Rotor Tail-sitter
J. Bain, K. Collins, Georgia Institute of Technology

 

Aerodynamic and Acoustic Test of a United Technologies Model Scale Rotor at DNW
Yung H. Yu, Sandy R. Liu, Aeroflightdynamics Directorate, US Army AVSCOM; Anton J. Landgrebe, Peter F. Lorber, United Technologies Research Center; Michael J. Pollack, Sikorsky Aircraft Div., UTC; Ruth M. Martin, NASA Langley Research Center; and Dave E. Jordan, NASA Ames Research Center

 

Aerodynamic And Aeroacoustic Layout Of The ATR (Advanced Technology Rotor)
Marius Bebesel, Eurocopter; G?nther Polz, Eurocopter; Eberhard Sch?ll, Eurocopter

 

Aerodynamic and Aeroacoustic Prediction Methodologies with Application to the HART II Model Rotor
Gaurav Gopalan, Jayanarayanan Sitaraman, James D. Baeder Fredric H. Schmitz, University of Maryland

 

Aerodynamic And Dynamic Design And Development Of The Main Rotor Of The YAH-64 Advanced Attack Helicopter
Kenneth B. Amer; James R. Neff; Sally V. LaForge; Ray W. Prouty

 

Aerodynamic And Dynamic Models For Rotor Load Prediction - Application To New Generation Blades
Guilhem LEBEL, EUROCOPTER; Bernard BENOIT, EUROCOPTER; Regis DUFOUR, LaMCoS - Universit? de Lyon; Georges JACQUET RICHARDET, LaMCoS - Universit? de Lyon

 

Aerodynamic and Numerical Issues for Coupling CFD into Comprehensive Rotorcraft Analysis
Lee, C. S. and Saberi, H., Advanced Rotorcraft Technology, Inc.; Ormiston, R. A., ATCOM

 

Aerodynamic and Wake Methodology Evaluation Using Model UH-60A Experimental Data
M.S. Torok and C.R. Berezin, Sikorsky Aircraft Div., UTC

 

Aerodynamic and Weight Efficiency of High Speed Rotorcraft Configurations
Troy Gaffey, AVX Aircraft Co.

 

Aerodynamic Characteristics of Model Rotors: The performance Prediction with Scaled Models
Tomoharu Fujino, Nagoya Aerospace Systems Works; Hiroyuki Arakawa, Yusaku Baba, and Tatsuo Motohashi, Nihon University

 

Aerodynamic Characteristics Of Two Rotary Wing UAV Designs
Henry E. Jones, Oliver D. Wong, Kevin W. Noonan, Deane G. Reis, Brendon D. Malovrh, NASA

 

Aerodynamic Considerations of Stopping a Rotor in Flight
Prouty, R. W. and Donham, R. E., Lockheed-California Company

 

Aerodynamic Design Considerations for Micro-Rotorcraft
Gray, Nate; Kim, J.; Koratkar, Nikhil

 

Aerodynamic Design of a Coanda Induced Force and Thruster Antitorque System
H. Velkoff, Sterling Federal Systems and C. Tung, U.S. Army Aeroflightdynamics Directorate

 

Aerodynamic Design of a New Affordable Main Rotor for the Apache Helicopter
Charles, Bruce; Hassan, Ahmed; JanakiRam, Ram; Smith, Roger

 

Aerodynamic Design of Advanced Rotors With New Tip Shapes
J.J. Philippe, ONERA & A. Vuillet, Aerospatiale

 

Aerodynamic Design of Helicopter Rotor Blade in Forward Flight Using Response Surface Methodology
Sun, Hyosung; Kim, Yushin; Lee, Soogab; Lee, Dongho

 

Aerodynamic Design of Helicopter Rotors for Reduced Brownout
Glen R. Whitehouse, Daniel A. Wachspress and Todd R. Quackenbush, Continuum Dynamics, Inc.

 

Aerodynamic Design of Helicopters for Reduced Brownout
G.R. Whitehouse, D.A. Wachspress, and T.R. Quackenbush, Continuum Dynamics, Inc.

 

Aerodynamic Design of Nacelle-Mounted Sails for Enhanced Tiltrotor Aircraft Performance
Michael A. McVeigh, Edward T. Meadowcroft, Robert F. Maciolek, Boeing Defense & Space Group

This paper was not submitted in time to be included in the printed Proceedings.

 

Aerodynamic Design Of The BA609 Civil Tiltrotor
Ted Trept, Bell Helicopter Textron, Inc.

 

Aerodynamic Design of the Sikorsky S-76 Helicopter
Fradenburgh, Evan A., Sikorsky Aircraft

 

Aerodynamic Design of the Sikorsky X2 Technology Demonstrator Main Rotor Blade
Bagai, Ashish

 

Aerodynamic Design of the V-22 Osprey Proprotor
Farrell, M. K, Bell Helicopter Textron, Inc.

 

Aerodynamic Design of the XV-15 Advanced Composite Tilt Rotor Blade
M.A. McVeigh & H.J. Rosenstein, Boeing Vertol Company

 

Aerodynamic Design Optimization of a Variable Diameter Tilt Rotor
Steven D. Larsen, McDonnell Douglas Helicopter Systems

 

Aerodynamic Design Optimization of Helicopter Rotor Blades Including Airfoil Shape
Vu, Anh

 

Aerodynamic Design Optimization of Proprotors for Convertible Rotor Concepts
Conor Stahlhut and J. Gordon Leishman, University of Maryland

 

Aerodynamic Design Rationale for the Fan-in-Fin on the S-67 Helicopter
David R. Clark, Sikorsky Aircraft

 

Aerodynamic Design Study of an Advanced Active Twist Rotor
M. Sekula, M. Wilbur, W. Yeager, US Army VTD

 

Aerodynamic Development of a Forebody Strake for the V-22 Osprey
Michael A. McVeigh and John Liu, Boeing Defense & Space Group, Heli. Div. and Tom Wood, Bell Helicopter Textron, Inc.

 

Aerodynamic Development of the Tiger Helicopter
Alain Cassier, Eurocopter SA, Roland Weneckers, Eurocopter Duetschland, Jean-Marc Pouradier, Eurocopter France

 

Aerodynamic Efficiency Potentials of Rotary Wing Aircraft
Evan A. Fradenburgh

 

Aerodynamic Evaluation of Miniature Trailing-Edge Effectors for Active Rotor Control
Matalanis, Claude; Min, Byung-Young; Opoku, Daniel; Sankar, Lakshmi; Wake, Brian; Yeshala, Nandita

 

Aerodynamic Evaluation of the V-22 Osprey Wing Section
J.C. Narramore, M.K. Farrell, Bell Helicopter Textron, W.K. Grauer, Boeing Defense & Space Group

 

Aerodynamic Investigations on a Helicopter Main Rotor Hub
Vogel, Florian

 

Aerodynamic Limitations of the UH-60A Rotor
Colin P. Coleman, NASA Ames; William G. Bousman, ATCOM

 

Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency
C.W. Acree, Jr., Ames Research Center

 

Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency
C.W. Acree, Jr., Ames Research Center

 

Aerodynamic Models and the Off-Axis Response
H.C. Curtiss, Jr., Princeton University

 

Aerodynamic Models and the Off-Axis Response
H.C. Curtiss, Jr., Princeton University

 

Aerodynamic Optimization of a Coaxial Proprotor
J.G. Leishman, S. Ananthan, University of Maryland

 

Aerodynamic Optimization Study of a Coaxial Helicopter Rotor
Leishman, J. Gordon; Syal, Monica

 

Aerodynamic Parameters That Affect Compressor Erosion in Gas Turbine Engines
R. M. Wood, Allison Div., GM Corp.; and R. M. Gaertner, NASC

 

Aerodynamic Performance Modeling of Ducted Fans and Shrouded Propellers for Preliminary Design
Conor Stahlhut, Boeing

 

Aerodynamic Performance of a 27-Percent-Scale AH-64 Wind-Tunnel Model with Baseline/Advanced Rotor Blades
H.L. Kelley and J.C. Wilson, Army Structures Laboratory, AVSCOM

 

Aerodynamic Performance of a Hovering Micro-Rotor in Confined Environment
Thierry Jardin, Sebastien Prothin, Cristian Garcia-Magana, ISAE Supaero

 

Aerodynamic Response of a Hovering Rotor to Ramp Change in Pitch Input
Brown, Richard; Duraisamy, Karthikeyan

 

Aerodynamic Results of a Pressure-Instrumented Model Rotor Test at the DNW
P.F. Lorber, United Technologies Research Center

 

Aerodynamic Results of a Pressure-Instrumented Nodal Rotor Test at the DNW
Lorber, Peter F., United Technologies

 

Aerodynamic Rig Test Results of an Advanced Small Engine Power Turbine
Spring, Samuel D.; Weider, Lee A.; Kinney, Stephen P.

 

Aerodynamic Shape Optimization for Alleviating Dynamic Stall Characteristics of Helicopter Rotor Airfoil
Qing Wang and Qi-jun Zhao and Qi Wu, Nanjing University of Aeronautics and Astronautics

 

Aerodynamic Shape Optimization of a Helicopter Main Rotor Hub Beanie Using Advanced Multi-Objective Evolutionary Algorithms
Lorenzo Dal Mas and Ernesto Benini, University of Padua; Rita Ponza, HIT09

 

Aerodynamic Shape Optimization of Hovering Rotors Using a Discrete Adjoint of the RANS Equations
Dumont, Antoine; Huberson, Serge; Le Pape, Arnaud; Peter, Jacques

 

Aerodynamic Shape Optimization of Rotor Airfoil Using a Viscous Continuous Adjoint Method
Wu Qi, Zhao Qi-Jun, Wang Qing, Nanjing University of Aeronautics and Astronautics

 

Aerodynamic Shape Optimization of Rotor Blades in Hover Using Unstructured Meshes
Kwon, Oh Joon; Lee, Sang Wook

 

Aerodynamic Studies of High Advance Ratio Rotor Systems
Todd Quackenbush, Continuum Dynamics, Inc; Daniel Wachspress, Continuum Dynamics, Inc; Robert McKillip, Jr., Continuum Dynamics, Inc; Marc Sibilia, Continuum Dynamics, Inc

 

Aerodynamic Study of the EC135 Fenestron in Hovering Flight Conditions by Means of CFD
D'Alascio, Alessandro; Kau, Hans-Peter; Kirstein, Sirka; Le Chuiton, Frederic; Mouterde, Edith; Sudre, Laurent

 

Aerodynamic Topology Design for Rotor Airfoils via Genetic Algorithm
D. W. Fanjoy and W. A. Crossley, Purdue University

 

Aerodynamic/Structural/Acoustic Prediction of HART II Rotor Using Weakly Coupled CFD-CSD Analysis
Aoyama, Takashi; Kwak, Jin-sung; Lee, Hyun-ku; Shin, SangJoon; Yang, Choongmo

 

Aerodynamics And Acoustics Of Blade-Vortex Interaction Using An Independently Generated Vortex
C. Kitaplioglu and F.X. Caradonna, NASA

 

Aerodynamics and Aeroacoustics of Rotating Transonic Flow Fields
J.W. Rutherford, U.S. Military Academy

 

Aerodynamics and Lifting Performance of a Quad Tilt Rotor in Ground Effect
Radhakrishnan, Anand; Schmitz, Fredric

 

Aerodynamics of a Rotor with a Solid Disc in Hover
Christopher Mesrobian, Demetri Telionis, Virginia Polytechnic Institute and State University

 

Aerodynamics of Helicopter Flight Near the Ground
P.F. Sheridan and W. Wiesner

 

Aerodynamics of Micro-Rotors in Confined Environments
Thierry Jardin, Sebastien Prothin, Cristian Garcia Magana, ISAE Supaero

 

Aeroelastic Analysis of a Composite Bearingless Rotor in Forward Flight with Improved Warping Modeling
Anita L. Tracy and Inderjit Chopra, University of Maryland at College Park

 

Aeroelastic Analysis of Rotor Blades Using Nonlinear Fluid/Structure Coupling
H. Murty, C. Bottasso, M. Dindar, M. Shephard, O. Bauchau, Rensselaer Polytechnic Institute

 

Aeroelastic Analysis Of The NASA/ARMY/MIT Active Twist Rotor
W. Keats Wilkie, NASA Langley Research Center; Matthew L. Wilbur, NASA Langley Research Center; Paul H. Mirick, NASA Langley Research Center; Carlos E. S. Cesnik, Massachusetts Institute of Technology; SangJoon Shin, Massachusetts Institute of Technology

 

Aeroelastic and Structural Analysis of Ducted Composite Rotors in Edgewise Flight
Smith, Edward; Zhang, Jianhua

 

Aeroelastic Behavior of Composite Rotor Blades with Swept Tips
K. Yuan, P.P. Friedmann, and C. Venkatesan, University of California, L.A.

 

Aeroelastic Characteristics Analysis of Helicopter Rotors Based on CFD/CSD Coupling Method
Wang Junyi, Zhao Qijun, Xiao Yu, Nanjing University of Aeronautics and Astronautics

 

Aeroelastic Characteristics Of Composite Bearingless Rotor Blades
Richard L. Bielawa

 

Aeroelastic Considerations for CSD-CFD Coupling
M.J. Laurita, M.J. Smith, and O.A. Bauchau, Georgia Institute of Technology

 

Aeroelastic Considerations For Rotorcraft Primary Control With On-Blade Elevons
Robert A. Ormiston, Ames Research Center

 

Aeroelastic Considerations Fur Torsionally Soft Rotors
Wayne R. Mantay and William T. Yeager, Jr., NASA/Langley Research Center

 

Aeroelastic Model Helicopter Rotor Testing In The Langley TDT
Wayne R. Mantay, William T. Yeager, Jr., M-Nabil H. Hamouda, Maj. Robert G. Cramer, Jr., Chester W. Langston, NASA Langley Research Center

 

Aeroelastic Modeling of Large Wind Turbines
Peretz Friedmann, University of California

 

Aeroelastic Modeling of Swept Tip Rotor Blades Using Finite Elements
R. Celi and P. Friedmann, UCLA

 

Aeroelastic Optimization of a Helicopter Rotor
J.W. Lim and I. Chopra, University of Maryland

 

Aeroelastic Optimization of a Helicopter Rotor with Composite Tailoring
Ranjan Ganguli and Inderjit Chopra, University of Maryland

 

Aeroelastic Optimization of an Advanced Geometry Composite Helicopter Rotor
Ranjan Ganguli and Inderjit Chopra, University of Maryland

 

Aeroelastic Response of Composite High-Speed Rotorcraft Blade with Non-uniform Cross Section in Unsteady Subsonic Compressible Flow
Jaber Javanshir Hasbestan, National Center for Computational Engineering, Touraj Farsadi, METU university

 

Aeroelastic Response of Composite High-Speed Rotorcraft Blade with Non-uniform Cross Section in Unsteady Subsonic Compressible Flow
Jaber Javanshir Hasbestan, National Center for Computational Engineering, Touraj Farsadi, METU university

 

Aeroelastic Response Of Swept Tip Rotors Including The Effects Of BVI
Marino de Terlizzi, Mechanical and Aerospace Engineering Department University of California; Peretz P. Friedmann, Mechanical and Aerospace Engineering Department University of California

 

Aeroelastic Simulation of Maneuvering Rotorcraft
Carlo L. Bottasso, Georgia Institute of Technology; Alessandro Croce, Politecnico di Milano

 

Aeroelastic Stability Analysis of a Composite Blade
C.-H. Hong and I. Chopra, University of Maryland

 

Aeroelastic Stability Analysis of Hingeless Rotor Helicopters in Forward Flight Using Blade & Airframe Normal Modes
R.T. Lytwyn, Boeing Vertol Company

 

Aeroelastic Stability Characteristics of a V/STOL Tilt-Rotor Aircraft with Hingeless Blades: Analysis and Test Correlation
H. R. Alexander and L. M. Hengen, Boeing Vertol Co. and W. J. Weiberg, NASA - Ames Res. Center. (Standby)

 

Aeroelastic Stability Flight Testing of the BA609 Tiltrotor
Johnson, Casey; Maddali, Rangacharylulu

 

Aeroelastic Stability for Straight and Swept-Tip Rotor Blades in Hover and Forward Flight
Thomas H. Maier, AVRDEC; David L. Sharpe, AVRDEC; Anita I. Abrego, NASA

 

Aeroelastic Stability of a Four-Bladed Semi-Articulated Soft-Inplane Tiltrotor Model
Brown, R.; Corso, L.; Kvaternik, R.; Langston, C.; Nixon, M.; Piatak, D.; Singleton, J.

 

Aeroelastic Stability of an Extremely Exible, Variable-diameter Rotor in Hover
Jérôme Sicard, Jayant Sirohi, University of Texas at Austin

 

Aeroelastic Stability of an Extremely Exible, Variable-diameter Rotor in Hover
Jérôme Sicard, Jayant Sirohi, University of Texas at Austin

 

Aeroelastic Stability Of Complete Rotors With Application To A Teetering Rotor In Forward Flight
Joseph Shamie; Peretz Friedmann

 

Aeroelastic Stability Of Modern Bearingless Rotors - A Parametric Investigation
Khanh Q. Nguyen, NASA Ames

 

Aeroelastic Stability of the McDonnell Douglas Advanced Bearingless Rotor
Khanh Nguyen, NASA Ames Research Center; Michael McNulty, Vaidyanathan Anand and Dan Lauzon, McDonnell Douglas Helicopter Company

 

Aeroelastic Tailoring for Stability Augmentation and Performance Enhancements of Tiltrotor Aircraft
Mark W. Nixon, Langley Reasearch Center; David J. Piatak, Langley Research Center; Lawrence M. Corso, Bell Helicopter Textron, Inc.; David A. Popelka, Bell Helicopter Textron, Inc.

 

Aeroflightdynamics Directorate: Capabilities and Role in Army Aviation S&T
Dick Spivey, US Army

 

Aeromechanic Considerations in Development of the Bell-Agusta 609 Civil Tiltrotor
Ross Menger, Bell Helicopter

 

Aeromechanical Analysis of a Slowed Rotor at High Advance Ratios using a Hybrid Methodology
Ritu P. Marpu, and Lakshmi N. Sankar, Georgia Institute of Technology

 

Aeromechanical Analysis of a Slowed Rotor at High Advance Ratios using a Hybrid Methodology
Ritu P. Marpu, and Lakshmi N. Sankar, Georgia Institute of Technology

 

Aeromechanical Analysis Tools for Design and Simulation of VTOL UAV Systems
Boschitsch, Alexander H.; Quackenbush, Todd R.; Solomon, Christine L.; Wachspress, Daniel A.

 

Aeromechanical Modeling of Active Trailing Edge Devices
Oliver Dieterich, Boris Grohmann, and Christoph Maucher, EUROCOPTER Deutschland GmbH (ECD)

 

Aeromechanical Modeling of Active Trailing Edge Devices
Oliver Dieterich, Boris Grohmann, and Christoph Maucher, EUROCOPTER Deutschland GmbH (ECD)

 

Aeromechanical Modeling Of Smart Composite Rotor Blade For Vibration Reduction
Aditi Chattopadhyay, Department of Mechanical and Aerospace Engineering Arizona State University; Qiang Liu, Department of Mechanical and Aerospace Engineering Arizona State University; Haozhong Gu, Department of Mechanical and Aerospace Engineering Arizona State University

 

Aeromechanical Stability and Response of Helicopters with Interblade Elastomeric Dampers
Brackbill, Christian R.; Smith, Edward C.; Lesieutre, George A.

 

Aeromechanical Stability and Response of Helicopters with Interblade Elastomeric Dampers
Christian R. Brackbill, Edward C. Smith, and George A. Lesieutre, The Pennsylvania State University

 

Aeromechanical Stability of a Full-Scale Hingeless Rotor in Hover
R.L. Peterson and W. Warmbrodt, NASA Ames Research Center, and J. Hoover, Boeing Vertol Company

 

Aeromechanical Stability of Helicopters with Composite Rotors in Forward Flight
E.C. Smith and I. Chopra, University of Maryland

 

Aeromechanics Analysis of a Compound Helicopter
H. Yeo, W. Johnson, Ames Research Center

 

Aeromechanics Analysis of a Heavy Lift Slowed-Rotor Compound Helicopter
Hyeonsoo Yeo, AMRDEC; Wayne Johnson, NASA

 

Aeromechanics and Aeroacoustic Predictions of the Boeing SMART Rotor Using Coupled CFD/CSD Analysis
Bain, Jeremy; Brentner, Kenneth; Potsdam, Mark; Sankar, Lakshmi

 

Aeromechanics Challenges for Tilting Propellor/Rotor Small VTOL UAS Package Delivery
Daniel P. Schrage, Matt Brown (Georgia Institute of Technology) and Don Shaw (Advanced Tactics, Inc.)

 

Aeromechanics Challenges for Tilting Propellor/Rotor Small VTOL UAS Package Delivery
Daniel P. Schrage, Matt Brown (Georgia Institute of Technology) and Don Shaw (Advanced Tactics, Inc.)

 

Aeromechanics Design for Vertical Lift (San Francisco, CA, Jan. 20-22, 2016)
various (49 papers and program)

Format: PDF.

Papers (PDF) are also available individually.

 

Aeromechanics Design With Non-Contiguous Hybrid Methodologies
Kevin Jacobson, Amanda Grubb, and Marilyn Smith (Georgia Institute of Technology)

 

Aeromechanics for a High Advance Ratio Coaxial Helicopter
Joseph Schmaus and Inderjit Chopra, University of Maryland

 

Aeromechanics of a Variable-Radius Rotor
Graham Bowen-Davies and Inderjit Chopra, University of Maryland

 

Aeromechanics of a Variable-Speed Rotor
Graham Bowen-Davies, University of Maryland; Inderjit Chopra, University of Maryland

 

Aeromechanics of the SMART Active Flap Rotor
Friedrich K. Straub and V.R. Anand, The Boeing Company

 

Aeronautical Design Standard - 33 (ADS-33) … Past, Present, and Future
Chris L. Blanken, Mark B. Tischler, Jeff A. Lusardi, Christina M. Ivler, U.S. Army

 

Aeronautical Design Standard 79-B Handbook For Condition Based Maintenance On Us Army Aircraft
William Lewis, Gail Cruce, Jane Parkins, US Army, AMRDEC

 

Aeroservoelastic Analysis of Rotorcraft-Pilot Coupling: A Parametric Study
Gennaretti, Massimo; Masarati, Pierangelo; Quaranta, Giuseppe; Serafini, Jacopo

 

Aerospace Fiber Optic Manufacturing
Mark W. Rowland, Sikorsky Aircraft Corporation; Curtis R. Taylor, Mechanical Engineering University of Maryland

 

Aerostructural Optimization of Winglets
Shahriar Khosravi, David W. Zingg, University of Toronto

 

Aerostructural Optimization of Winglets
Shahriar Khosravi, David W. Zingg, University of Toronto

 

Afforability Means Not Only the Low Prices
Antoni Gnot, WSK PZL-Rzeszow SA

 

Affordability And Performance In Rotorcraft Design A Guide For The Perplexed
Mayaard L. Marquis, George Price, Sikorsky Aircraft Corporation

 

Affordability Metrics Introduction and Example for the FTR/JTR
Schrage, D. P.

 

Affordability Through Intelligent Engine Health Management
Dr. Link Jaw, Scientific Monitoring, Inc.

 

Affordable CFD Simulations of Rotors in Forward Flight - A Feasibility Study with Future Application to Vibrational Analysis
Van der Ven, H.

 

Affordable Flight Simulation in an Educational Environment
Cerny, Jeff; Landrum, D. Meyer, Austin; Warden, Lance

 

Affordable Helicopter Avionics Bay Door In Thermoplastic Composites
Pierre H. Jouin, Boeing Mesa; Thomas G. Klingler, Boeing Mesa; Alan D. Stemple, Boeing Mesa

 

Affordable Rotorcraft Acquisition, Testing & Training
Dean Carico, Naval Air Warfare Center

 

Affordable Thermoplastic Structures
D. Orlino, U.S. Army AATD (ATCOM), N. Caravasos, Boeing Defense & Space Group, Heli Div., and M. Pasanen, Automated Dynamics Corporation

 

AFP Monocoque Composite Tailboom Full Scale Fatigue Testing
Alain Colle and Maxime Lapalme and Pierre Drouin, Bell Helicopter; C. Andre Beltempo and John E. Rogers and Robert. S. Rutledge, National Research Council Canada

 

AFSOC Goes to War: Scud Running in the CV?22
Jon S. Tatro, Bell Helicopter Textron, Inc.; Maj Lee Pera and Lt Col Rick LeMaster, Air Force Special Operations Command (AFSOC)

 

Aggregate Analysis of Health and Usage Monitoring System Data on Naval Rotorcraft
Brian L. Fuller, NSWCCD; Joel Walker, Quadelta, Inc; David Haas, NSWCCD; Trisha Shields, NSWCCD

 

Aggregate Analysis of Health and Usage Monitoring System Data on Naval Rotorcraft
Brian L. Fuller, NSWCCD; Joel Walker, Quadelta, Inc; David Haas, NSWCCD; Trisha Shields, NSWCCD

 

Aggregate Analysis of Health and Usage Monitoring System Data on Naval Rotorcraft
Brian L. Fuller, NSWCCD; Joel Walker, Quadelta, Inc; David Haas, NSWCCD; Trisha Shields, NSWCCD

 

Aggressive Maneuvering for Obstacle Avoidance with Envelope Protection for Autonomous UAVs
Jongki Moon, J.V.R. Prasad, Georgia Institute of Technology

 

Agricultural Helicopters
H.E. Lemont, Bell Helicopter Textron

 

Agricultural Uses of The Helicopter
Frank H. Kelley, Jr., Bell Aircraft Corporation

 

Agricultural Uses of The Helicopter
Frank H. Kelley, Jr., Bell Aircraft Corporation

 

Agusta A109 POWER, CAT A Take Off and Landing Manuevers Real Time Presentation Using a Differential GPS System
B. Paggi, M. Bonetti, and D. Porrini, AGUSTA

 

Agusta A109E and GPS WAAS: Poised for Takeoff
Dioli, Marco; Haney, Clayton W.; Hilmer, Jeffrey

 

Agusta's Integrated Technology For Next Century Developments
Pietro Alli, AGUSTA- Finmeccanica Company

 

AgustaWestland
William Schneider, Jr.

 

AgustaWestland Project Zero [Presentation]
James Wang, AgustaWestland

 

AH-1G Flight Vibration Correlation Using Nastran and The C81 Rotor/Airframe Coupled Analysis
R.V. Dompka and J.J. Corrigan, Bell Helicopter Textron, Inc

 

AH-1W MSC/NASTRAN Finite Element Analysis Correlation
Michael Seifert, Bell Helicopter Textron, Inc.

 

AH-56A (AMCS) Compound Helicopter Vibration Reduction
W. D. Anderson and E.R. Wood, Lockheed-California Co.

 

AH-56A Compound Helicopter Icing Spray-Rig Tests
A.M. Petach, J.B. Werner, F. Mastroly, Lockheed-California Company

 

AH-56A Vehicle Development
J. F. Johnston and J. R. Cook, Lockheed-Calif. Co.

 

AH-64 Apache Modernization
Robert Johnston, US Army

 

AH-64 Apache: Army Flight Test Update
Major Allen L. Peterson, Major Patrick J. Oarman, and Major Daniel G. Wolfe, U.S. Army Aviation Technical Test Center

 

AH-64 Composite Aft Fuselage Ground Test Load Derivation, Execution, and Results Correlation
Lisa Gamache, The Boeing Company; Dennis McCarthy, The Boeing Company; Richard Weisenburger, The Boeing Company

 

AH-64 External Air Particle Separator (EAPS) Design and Performance
Keith E. Boyd, Ph,D., and Robert K. Burgess, McDonnell Douglas Helicopter Company (INSERT)

 

AH-64 Injury Reduction Potential with Cockpit Airbags and Optical Relay Tube Removal
B. Joseph McEntire, Samuel G. Shannon, Christopher Smith (MAJ), and George Crockatt, U. S. Army

 

AH-64 Prototype Composite Tailboom
Ellerbeck, Nick; McCarthy, Dennis; Pyle, Glenn; Schrieber, Keith; Zwick, Robin

 

AH-64 Prototype Composite Vertical Stabilizer with an Embedded Sensor Network
Ayers, Laura; Bender, Matthew; Federici, John; McCarthy, Dennis

 

AH-64 Shake Test and Correlation with NASTRAN Finite Element Model Predictions
M. Toossi, D. Ferg, R. Weisenberger and F. Straub, McDonnell Douglas Helicopter Company

 

AH-64 Tail Rotor Balance Influenced by Stabilator Natural Frequency
Ronald Bednarczyk, U.S. Army; Stanley Graves, Camber Corporation

 

AH-64A & D Apache
COL Derek Paquette

 

AH-64A Apache Helicopter Reliability, Availability, Maintainability/Logistics RAM/LOG Data System
H.E. Pohlenz, McDonnell Douglas Helicopter Co

 

AH-64A Apache, Development of Capabilities for the Aerial Combat Role
J.A. Buresh, C.A. Parlier, and W . E . Wilson, McDonnell Douglas Helicopter Co.

 

AH-64A Contractor Logistics Support: The Contractors' Perspective
J. Reagan and J. Wood, McDonnell Douglas Helicopter Co.

 

AH-64A Production Line Automatic Test Equipment
J.B. Davies, Hughes Helicopters, Inc. and D. Talley, Design Engineering Laboratories, Inc.

 

AH-64A Rotating Load Usage Monitoring From Fixed System Information
C. T. Gunsallus, Kaman Aerospace Corporation; Eric Robeson, AVSCOM

 

AH-64D Apache Longbow Structural Usage Monitoring System (ALB SUMS)
Lu, Yi; Christ, Richard A.; Puckett, Tim A.; Teal, Richard S.; Thompson, Bruce

 

AH-64D Main Transmission Accessory Drive Spur Gear Installation Fault Detections
Jonathan Keller, Damian Carr, US Army RDECOM; Frances Love, US Army Apache Program Management Office; Paul Grabill, Honeywell Aerospace; Hieu Ngo, Perumal Shanthakumaran, The Boeing Company

 

AH-64D Swashplate Test Stands: Improving Understanding of Component Behavior in Rotorcraft Swashplates through External Sensors
Travis Edwards, Thomas Hartmann, Andrew Patterson, Samuel Bernstel, Dr. Joshua Tarbutton, Dr. Abdel Bayoumi, University of South Carolina; Damian Carr, AED; MG. Lester Eisner, SC National Guard

 

AH-64D Swashplate Test Stands: Improving Understanding of Component Behavior in Rotorcraft Swashplates through External Sensors
Travis Edwards, Thomas Hartmann, Andrew Patterson, Samuel Bernstel, Dr. Joshua Tarbutton, Dr. Abdel Bayoumi, University of South Carolina; Damian Carr, AED; MG. Lester Eisner, SC National Guard

 

AH-64D/AH-64E Apache Update
Brian Stehle, US Army

 

AH-6: Creating an Agile Software Product Line Architecture
Andrew Augenstein, The Boeing Company

 

AH64A Reliability and Maintainability Improvement Program
Albert V. Schaff Kenneth M. Becker, McDonnell Douglas Helicopter Systems

 

AH64D Apache Longbow Airframe Dynamic Testing
Richard Weisenburger, The Boeing Company; Murugappan Meyyappa, The Boeing Company; Ray Sundar, The Boeing Company; Thomas Collison, The Boeing Company

 

AHIP: The OH-58D From Conception to Production
F.D. Harris, Bell Helicopter Textron, Inc

 

AHS 57th Annual Forum and Technology Display 9 - 11 May 2001, Washington, DC, USA
Krzysztof Gajda, Warsaw University of Technology; Janusz Narkiewicz, Warsaw University of Technology

 

AHS and YOU: Partners for the Future
Mike Hirschberg, AHS International

 

AHS Fifth Decennial Specialists' Meeting on Aeromechanics (San Francisco, CA, Jan. 22-24, 2014)
various (43 papers and program)

Format: PDF.

Papers (PDF) are also available individually.

 

AHS Fourth Decennial Specialists' Conference on Aeromechanics (San Francisco, CA, Jan. 21-23, 2004)
various (52 papers and 5 briefs)

Format: HTML

 

AHS Future Vertical Lift Aircraft Design Conference (San Francisco, CA, Jan. 18-20, 2012)
various (25 papers and 8 briefs)

Format: PDF, PPT, movies.

Papers (PDF) are also available individually.

 

AHS Journal - 50th Anniversary
J. Gordon Leishman, AHS International

 

AHS Specialists' Conference on Aeromechanics (San Francisco, CA 2010, Jan. 20-22, 2010)
various (59 papers)

Format: PDFs

 

AHS Specialists' Conference on Aeromechanics (San Francisco, CA, Jan. 23-25, 2008)
various (54 papers)

Format: PDFs

 

AHS Student Chapter
Sue O?Brien, Dave Simmons, and Jake Keplinger, University of Alabama in Huntsville

 

AHS Systems Engineering Specialists CORE Demo
Don Estes, Program Executive Office

 

AHS/RAeS International Meeting On Rotorcraft Noise And Rotor Fluid Dynamics - An Overview on Practical Application of Helicopter Noise Certification Rules
Estival and F. d'Ambra, Aerospatiale

 

AHS/RAeS International Meeting On Rotorcraft Noise And Rotor Fluid Dynamics - An Overview on Practical Application of Helicopter Noise Certification Rules
Estival and F. d'Ambra, Aerospatiale

 

Air Alignment for the Base Inertial Navigation System - LINS 300
Richard H. W. Reilly, British Aerospace (Systems & Equipment), Ltd.

 

Air Combat Tactics for the Evaluation of Rotorcraft Characteristics in the Low Air War of 2010
J.V. Mackmull, Defense Consultant and D.L. Green, STARMARK Corp.

 

Air Force Testing and Evaluation of Helicopters
Capt. Wayne W. Eggert, Wright-Patterson AFB

 

Air Vehicle Diagnostic System Technology Demonstration Program
David J. Haas, Naval Surface Warfare Center; Carl G. Schaefer, Jr., FutureLink, Inc.

 

Air-Ground Mobility: Discovering Qualities of Vertical Maneuver Necessary to Project the Future Force
Frakes, Larry; Huber, Allen; Godwin, D. Brian

 

Air-Resonance Analysis of Hingeless Rotor in Hovering Flight Using a 3-D Interblade Unsteady Wake Model
K.M. Yoo, KlAT

 

Air-To-Air Combat Helicopter Development
J.M. McCollough, C. Stroncek, and H. Ward, Bell Helicopter Textron

 

Air-To-Air Combat Test IV (AACT IV) and the AACT Data Base
D.A. Skrinjorich and G.T. White, U.S. Army Aviation Applied Technology Dir.

 

Air-To-Air Starstreak - Integrating and Testing an Air Defense Missile in the Air-To-Air Role
Ryland Barlow, AVRDEC; Ronnie Harrison, Shorts Missiles Systems

 

Airborne and Ground Resonance of Hingeless Rotors
R. T. Lytwyn, and W. Miao, Boeing/Vertol, and W. Woitsch, Messerschmitt-Boelkow, GmbH

 

Airborne Flight Reporting System
Kaydon Stanzione, Praxis Technologies, Inc.

 

Airborne Flight Test Data Acquisition and Automatic Data Processing System for Helicopter Test and Development Program
F. Kreutz, Sikorsky Aircraft Div.

 

Airborne Integrated Monitoring System
A.H. Neubauer, Jr., Teledyne Controls

 

Airborne Manned Unmanned System Technology (AMUST) Program
LTC Allen L. Peterson, US Army; Mr. Kristopher F. Kuck, US Army

 

Airborne Manned Unmanned System Technology Baseline Program
Gary R Fayaud, Army Aviation Applied Technology Directorate

 

Airborne Video Recorder And Image Transceiver (AVRIT) - AH-64 Attack Helicopter Integration
Maj Christopher Smith, Flight Test Directorate

 

Aircraft Conceptual Design Trim Matrix Selection
John Preston, NASA Ames

 

Aircraft Condition Monitoring via an Electronic Kneeboard
Floyd Glenn, CHI Systems, Inc.; John Deaton, CHI Systems, Inc.; Charles Barba, CHI Systems, Inc.; Edward Popp, CHI Systems, Inc.; Carl Byington, Penn State University Applied Research Laboratory; Michael Good, Honeywell Laboratories

 

Aircraft Data Monitoring Systems
Tim Doucet, PHI, Inc.

 

Aircraft Data Monitoring Systems
Tim Doucet, PHI, Inc.

 

Aircraft Disassembly; Risks, Challenges and Opportunities Analysis
Hamidreza Zahedi, Christian Mascle, Pierre Baptiste, École Polytechnique de Montréal

 

Aircraft Disassembly; Risks, Challenges and Opportunities Analysis
Hamidreza Zahedi, Christian Mascle, Pierre Baptiste, École Polytechnique de Montréal

 

Aircraft Flow-Off Performance of De/Anti-Icing Fluid During Take-Off Under Cold Precipitation
Xiaofei Wang, Sylvie Bernardin, and Jean-Louis Laforte, Université du Québec

 

Aircraft Flow-Off Performance of De/Anti-Icing Fluid During Take-Off Under Cold Precipitation
Xiaofei Wang, Sylvie Bernardin, and Jean-Louis Laforte, Université du Québec

 

Aircraft Lighting Systems
J.F. Verney, Sikorsky Aircraft Division, United Technologies Corp

 

Aircraft Seat Certification by Analysis from a Regulatory Perspective
Joseph Pellettiere and David Moorcroft, Federal Aviation Administration

 

Aircraft Seat Certification by Analysis from a Regulatory Perspective
Joseph Pellettiere, David Moorcroft, Federal Aviation Administration

 

Aircraft Survivability Advances Against Hard to Detect Small Arms, RPG and MANPADS Threats
Torrey Deas, US Army AATD (RDECOM)

 

Aircraft Survivability Rating
Jordan Kaye, Sikorsky; Mark Robeson and Nathaniel Bordick, Aviation Applied Technology Directorate

 

Aircraft Wire Fault Detection and Isolation using Spread Spectrum Time Domain Reflectometry
Brian Drost, Impact Technologies, A Sikorsky Innovations Company; Bruce Thompson, U.S. Army Aviation Development Directorate; Mike Mastrianni, Sikorsky Aircraft

 

Airflow Hazard Visualization for Helicopter Pilots: Flight Simulation Study Results
Cecilia R. Aragon, Computational Sciences Division NASA Ames Research Center, Kurtis R. Long, US Navy Shipboard Rotorcraft Flight Test Group and NASA Ames Research Center

 

Airfoil Design and Rotorcraft Performance
Bousman, Williams G.

 

Airfoil Design for Helicopter Rotor Blades A Three-Dimensional Approach
Ahmed A. Hassan, Bruce D. Charles, McDonnell Douglas Helicopter Systems

 

Airfoil Design, Test and Evaluation for the V-22 Tilt Rotor Vehicle
J.C. Narramore, Bell Helicopter Textron

 

Airfoil Sections for Helicopter Rotors - A Reconsideration
Franklyn J. Davenport, and John V. Front, Boeing Co., Vertol Div.

 

Airframe Active Vibration-Based Damage Detection and Localization
Justin Long, The Pennsylvania State University; Stephen Conlon, Applied Research Laboratory

 

Airframe Aerodynamics of the CRW Demonstrator Aircraft in Hover with Winds
R.L. Smith, R. JanakiRam, The Boeing Company; S. Niazi, Sukra HeliTek, Inc.

 

Airframe and Propulsion Assessment of Light Helicopter Technologies (LHX)
K.A. Stanzione and R.F. Smith, Praxis Technologies Corp.

 

Airframe Condition Evaluation Corrosion Prevention and Control Evaluation
Duran, Don

 

Airframe Design of the S-76 Helicopter
W. Whiteside and J.D. Ray

 

Airframe Interference Effects On Rotorcraft BVI
Bruce D. Charles, The Boeing Company; Ahmed A. Hassan, The Boeing Company

 

Airframe Structural Integrity Management: A UH-60 Application and Demonstration
Andrew Brookhart and Preston Bates, Sikorsky Aircraft Corporation; Nathaniel Bordick, U.S. Army Aviation Development Directorate - AATD

 

Airframe Water Impact Analysis Using A Combined MSC/DYTRAN - DRI/KRASH Approach
Gil Wittlin, Dynamic Response, Inc.; Michael Smith, Ashish Sareen, Ph. D., Bell Helicopter Textron, Inc.; Marv Richards, Simula Government Products, Inc.

 

Airframe Water Impact Analysis Using a Local/Global Methodology
N. Pentec?te, DLR; C.M. Kindervater, DLR

 

Airloads Prediction for Flapping and Rotary Wing MAVs
Beerinder Singh, Inderjit Chopra, University of Maryland

 

Airloads Prediction of a UH-60A Rotor inside the 40- by 80-Foot Wind Tunnel
I. Chang, E. Romander, NASA Ames Research Center; M. Potsdam, H. Yeo, Aeroflightdynamics Directorate, U.S. Army RDECOM

 

Airplane Sizing For Electric Propulsion
Neal Willford, Textron Aviation

 

Airplane Sizing For Electric Propulsion
Neal Willford, Textron Aviation

 

Airworthiness in the Systems Engineering Process
William D. Lewis, AMRDEC

 

Airworthiness Integration Into Modern Systems Engineering for Complex Military Systems
Schrage, Daniel

 

Airworthiness of Complex Systems IMPACT Study
David Arterburn, RSESC

 

Airworthiness, CBM and HUMS Specialists' Meeting (Huntsville, AL, Feb. 11-13 2013)
various

 

Airworthiness, CBM and HUMS Specialists' Meeting (Huntsville, AL, Feb. 7-9 2011)
various

 

Airworthiness, CBM and HUMS Specialists' Meeting (Huntsville, AL, Feb. 9-11 2015)
various

 

Alexander A. Nikolsky Honorary Lectureship
David A. Peters, McDonnell Douglas

 

Algorithm Design of a Distributed Strap-down Inertial Navigation System for Unmanned Rotorcraft
Jiandong Guo, Yanguo Song, Nanjing University of Aeronautics and Astronautics

 

Algorithmic Icing Detection For The V-22 Osprey
Robert McKillip, Jr. Jeffrey Keller, Andrew Kaufman, Continuum Dynamics, Inc.

 

All Composite Helicopter Airframe Roof Structure
M.J. Rich & B.F. Kay, Sikorsky Aircraft Div., UTC

 

All-Electric Fuel and Oil Control System Demonstration on the T55 Engine
Richard Brauer, Theodore Busky and Robert Niebanck, Triumph Engine Control Systems

 

Alleviation of Dynamic Stall Induced Vibrations Using Actively Controlled Flaps
Depailler, Gilles; Friedmann, Peretz P.

 

Alleviation of Whirl-Flutter on Tilt-Rotor Aircraft Using Active Controls
J.M. Van Aken, Sterling Software

 

ALLFlight - A Synthetic Vision Sensor Suite with 'See-Through' Capability for Helicopter Applications
Thomas Lueken and Hans-Ullrich Doehler, German Aerospace Center

 

ALLFlight: A Full Scale Pilot Assistance Test Environment
Robin Lantzsch, Steffen Greiser, Jens Wolfram, Johannes Wartmann and Mario M?llh?user, Thomas L?ken, Hans-Ullrich D?hler and Niklas Peinecke, DLR

 

Allison T63 Regenerative Engine Program
Edward J. Privoznik

 

Along Side Analysis Of Type 23 Ship Motion As A Function Of Mechanical And Dynamic Limits Of An EH101-Like Helicopter Using The Landing Period Designator Helicopter Recovery Device
R. Bruce Lumsden, Defence Research Agency; Bernard Ferrier, Bombardier Inc.

This paper was not submitted in time to be included in the printed Proceedings.

 

Alterations of the Tip Vortex Structure From a Hovering Rotor Using Passive Tip Devices
Justin W. Russell and Lakshmi N. Sankar, Georgia Institute of Technology; Chee Tung, NASA Ames Research Center, Michael T. Patterson, Silicon Graphics/Cray Research, Inc.

 

Alternate Course Of Action Training For Helicopter Pilots
Rick Archer, Micro Analysis & Design, Inc.; Brett Walters, Micro Analysis & Design, Inc.; Jay Shively, Ames Research Center; Lynne Martin, Ames Research Center; Robert Dodd, Dodd Associates

 

Alternate Detail Part Design and Analysis: Topology, Size, and Shape Optimization of CH-47 Chinook Underfloor Structure
E. Hunter, Boeing

 

Alternative Human Machine Interface Display Concepts for Next Generation Military Rotorcraft
Faerber, Bob

 

Altitude and Ground Track Predicting Flight Path Marker Symbol for Rotorcraft Synthetic Vision Displays
Z.P. Szoboszlay, E.M. III, US Army

 

Aluminum Lithium Alloys - Processing and Properties
P.C. Inguanti, Sikorsky Aircraft Division, UTC

 

Aluminum Metal Matrix Composite Liner Testing
Bruce Hansen, Timothy Demers, Sikorsky Aircraft; Jason Fetty, Treven Baker, US Army

 

Amelioration of Blade Vortex Interaction Using Blade Tip Jets
Coton, Frank N.; Green, Richard B.; Early, Juliana M.; Price, Jennifer L.

 

America?s Incredible, Shrinking, Aging, Less Ready, Ever More Expensive Armed Forces
Winslow T. Wheeler, Center for Defense Information

 

American Helicopter Society (AHS) International The Vertical Flight Technical Society
Mike Hirschberg, AHS International

 

AMMI: Intelligent Support For Alarm Systems in Advanced Rotorcraft
James H. Hicinbothom, William Weiland, Thomas Santarelli, Clarence A. Fry, CHI Systems, Inc.; James W. Voorhees, Advanced Simulation Engineering; Allen L. Zaklad, Independent Consultant

 

AMRDEC Avionics Reference Embedded System (ARES)
David W. Boyett and H. Glenn Carter, AMRDEC; Ashley M. Denny, BAE Systems; Anthony L. Edwards, GTRI; Chris M. Kellow, DHPC; Jennifer J. Pittman, BAE Systems; Jason L. York, Intrepid

 

An ABC Status Report
A. Linden & A. Ruddell, Sikorsky Aircraft Division, UTC

 

An Accelerometer-Based Instrumentation System for Measurement of Helicopter Rotor Motion and Loads
R.M. McKillip, Jr., Continum Dynamics, Inc.

 

An Accurate Nonlinear Finite Element Analysis And Test Correlation Of A Stiffened Composite Wing Panel
D.D. Davis, Jr., U.S. Army; W.J. Stroud, NASA

 

An Active Fuzzy Control for Vibration Reduction of a Smart Rotor with Trailing-edge Flap
Yamin Wang, China Helicopter Research and Development Institute

 

An Adaptation of Model Analysis to the Computation of Steady Bending Loads on a Rotating Beam
J. Corrigan, G. Sadler and M. Yuce, Bell Helicopter Textron, Inc.

 

An Advanced Composite Tail Boom for the AH-1G Helicopter
H. Zinberg, Bell Helicopter Co.

 

An Advanced Fly-By-Wire Flight Control System Designed For Airborne Research - Concept To Reality
Fernando Dones, Boeing Rotorcraft Division; James B. Dryfoos, Boeing Rotorcraft Division; Donald L. McCorvey, Boeing Rotorcraft Division; William S. Hindson, NASA Ames Research Center

 

An Advanced Method for Predicting the Performance of Helicopter Propulsion System Ejectors
C.C. Folkman, McDonnell Douglas Helicopter Co.

 

An Advanced Program in Rotorcraft Design Education
V.L. Wells, A.T. Glinka, IV, D.H. Laananen, Arizona State University and J.W. Rutherford, McDonnell Douglas Helicopter Systems

 

An Advanced Rotorcraft Powerplant Optimization at Mission Level: Towards High Fidelity Engine Design Optimization
Fakhre Ali, Konstantinos Tzanidakis, Ioannis Goulos and Pachidis Vassilios, Cranfield University; Roberto d'’Ippolito, NOESIS Solutions

 

An Aeroacoustic Optimization Model - A Multiobjective, Multilevel Decomposition Based Optimization Technique
H. Tadghighi, The Boeing Company

 

An Aeroelastic Model Structure Investigation for a Manned Real-Time Rotorcraft Simulation
William D. Lewis, LTC., U.S. Army AATD

 

An Aeromechanical Stability Analysis for Bearingless Rotor Helicopters
Hodges, Dewey H., AVRADCOM

 

An Affordable Approach to Rotorcraft Vehicle Management Systems
Lee Graba, Cliff Miyaoi, Anthony Mangogna, Honeywell International

 

An Affordable Solution to Heavy Lift - CH-53X Future Stallion
James C. Garman, Sikorsky Aircraft Corporation

 

An Alternate Methodology for Harmonic Analysis of Flight Test Data
M. Meyyappa, McDonnell Douglas Helicopter Systems

 

An Alternative Approach for System Architecture Design
Germanetti Serge and Erwan Guillanton, Eurocopter

 

An Alternative Approach to Anomaly Detection in Health and Usage Monitoring Systems – Mixture Modeling
Dean Westerfield, Qinetiq North America, Inc.; Christopher Doktor, Frontier Technology, Inc.

 

An Alternative Approach to Anomaly Detection in Health and Usage Monitoring Systems – Mixture Modeling
Dean Westerfield, Qinetiq North America, Inc.; Christopher Doktor, Frontier Technology, Inc.

 

An Analysis Of Blade-Motion Stability For An Articulated Rotor
Julian L. Jenkins, Jr.

 

An Analysis Of Blade-Motion Stability For An Articulated Rotor
Julian L. Jenkins, Jr.

 

An Analysis of Grid Reduction for Solving Rotor Blade with CFD/Doublet Surface/Free Wake Coupling
Jang, Ji Seong; Lee, Duck Joo; Wie, Seong Yong

 

An Analysis of Helicopter Blade-Vortex Interaction Noise with Flight Path or Attitude Modification
Munsky, Brian; Gandhi, Farhan; Tauszig, Lionel

 

An Analysis Of HUMS Vibration Diagnostic Capabilities
Brian D. Larder, Stewart Hughes Limited

 

An Analysis of Pitch and Plunge Effects on Unsteady Airfoil Behavior
J.C. Tyler and J.G. Leishman, University of Maryland

 

An Analysis of the Helicopter Transfer Function to Predict Achievable Handling Characteristics of the Stabilized Helicopter
Edward Sterling Carter, Jr., Sikorsky Aircraft Division

 

An Analysis of the Stall Flutter Instability of Helicopter Rotor Blades
Carta, Franklin O., United Aircraft; Ham, Norman D., Massachusetts Institute of Technology

 

An Analysis Of Use Of Damage Tolerant Criteria For Helicopter Design
James Michael, Bell Helicopter Textron, Inc.; Bill Dickson, Bell Helicopter Textron, Inc.; Tom Campbell, Bell Helicopter Textron, Inc.

 

An Analysis Of “Vortex Ring State” Encounters From Flight Test Data With Application To An Onboard Warning System
R.W. Duren, M.A. Couch, and E.R. Wood, Naval Postgraduate School

 

An Analysis on High Speed Impulsive Noise of Transonic Helicopter Rotor
O. Rho and Y.S. Kim, Seoul National University

 

An Analytical And Experimental Evaluation Of Airfoil Sections For Helicopter Rotor Application
Gene J. Bingham and Kevin N. Noonan, NASA Langley Research Center

 

An Analytical Approach To The Determination Of Particle Trajectories In A S-Bend Duct With Experimental Verification
Murray I. Leitner

 

An Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces
Kenneth S. Brentner and F. Farassat, NASA Langley Research Center

 

An Analytical Formulation for Lifting Rotor Induced Power
Ormiston, Robert

 

An Analytical Method For Predicting Energy Absorption Capability Of Composite Stiffeners
A.O. Bolukbasi, McDonnell Douglas Helicopter Company; D.H. Laananen, Arizona State University

 

An Analytical Method To Predict Ideal H-V Boundary And C.D.P. Of Rotorcraft With Special Attention To The Application Of Optimalizing Techniques
Masaki Komoda, National Aerospace Laboratory

 

An Analytical Methodology For Category A Performance Prediction And Extrapolation
Eric Bernard Carlson, Bell Helicopter Textron, Inc.

 

An Analytical Model for a Nonlinear Elastomeric Lag Damper and its effect on Aeromechanical Stability in Hover
Farhan Gandhi and Inderjit Chopra, University of Maryland

 

An Analytical Model for Describing the Response of an Unsymmetrical Rotor
S. P. Viswanathan, A. W. Myers, and T.T. McLarty

 

An Analytical Study of a Multicycle Controllable-Twist Rotor
John L. McCloud III, NASA, Ames Research Center

 

An Analytical Study of Helicopter Handling Qualities in Hover
Richard P. Walton, and Robert L. Stapleford, Systems Technology, Inc.

 

An Analytical Study of Rotor Performance at High Forward Speeds
Franklin D. Harris

 

An Analytical Study of the Dynamics of VTOL Aircraft in Unsteady Flight
H. C. Curtiss, Jr., Princeton University

 

An Anechoic Wind Tunnel for the Investigation of the Main-Rotor/Tail-Rotor Blade Vortex Interaction
Con J. Doolan and Damien Leclercq, The University of Adelaide

 

An Anechoic Wind Tunnel for the Investigation of the Main-Rotor/Tail-Rotor Blade Vortex Interaction
Con J. Doolan and Damien Leclercq, The University of Adelaide

 

An Anglo-French Rotor Blade Stability Workshop Using Different Prediction Methods and Test Results
Stephen. A. Holton, West land Helicopters, Frederic Beroul, Eurocopter France, Didier Petot, O.N.E.R.A., William.R. Walker DRA Farnborough

 

An Application of a Polyamide Epoxy Adhesive to Airframe Structural Components
Raymond B. Krieger, Jr.

 

An Application of Knowledge-Based Engineering to Composite Tooling Design
S.L. Lewis and P.H. Jouin, McDonnell Douglas Helicopter Co.

 

An Applied and Theoretical Approach to the Development of a Twin Ducted Fan VTOL Aircraft
Speck, Michael, University of Canterbury; Buchholz, J?rg, Hoschschule Bremen; Sellier, Mathieu, University of Canterbury

 

An Approach for Experimental Characterization of Damage Processes in Thick Rotorcraft Composite Components
Brian Bouquillon, Sikorsky Aircraft Corporation, Mark Gurvich and Patrick Clavette and Prabhakar Rao, United Technologies Research Center

 

An Approach To Fatigue Damage Estimation Of Helicopter Rotating Components Using Computational Intelligence Techniques
Bruno Rocha, NRC - National Research Council Canada, Catherine Cheung and Julio Valdes and Anton Stefani and Matthew Li, National Research Council Canada

 

An Approach to Fault Diagnosis and Failure Prognosis of Spline Wear
Covington, Eric; Edwards, Derek; Ehinger, Ryan; Goldsmith, Jared; Khawaja, Taimoor; Sconyers, Chris; Vachtsevanos, George; Voulgaris, Zacharias

 

An Approach to Military Airworthiness Certification of a Previously Developed Helicopter from a Flying Qualities Perspective
Benjamin Kangas and Shawn Disarufino, The Boeing Company; Bram Renier, AgustaWestland

 

An Approach to Modeling The Effectiveness of MTI Radars in Detecting Dynamic RCS
Seals, Rupert L.; Stone, Ian G.

 

An Approach to Reducing Rotor-Body Coupled Roll Oscillations on the RAH-66 Comanche Using Modified Roll Rate Feedback
James B. Dryfoos, The Boeing Company; John Mayo, Sikorsky Aircraft; Bruce D. Kothmann, The Boeing Company

 

An Approach to Reducing Rotor-Body Coupled Roll Oscillations on the RAH-66 Comanche Using Modified Roll Rate Feedback
James B. Dryfoos, The Boeing Company; John Mayo, Sikorsky Aircraft; Bruce D. Kothmann, The Boeing Company

 

An Approach to STOVL Flight Testing
Paul Bevilaqua, Lockheed Martin Corporation

 

An Approach to the Aerodynamic Design of Optimum Rotors for Wind-Power Generators
Carl Rohrbach and Rose Worobel, UAC Hamilton Standard Div.

 

An Approach To The Determination Of Higher Harmonic Rotor Blade Stresses
H. Daughaday; J. Kline

 

An Architecture for Multi-Vehicle Autonomy with Small UAVS
Bamberger, R.; Bruzek, J.; Gilreath, H.; Gion, Tim; Grossman, K.

 

An Architecture-Based Approach for Modeling Hardware and Software
Hensley, Philip; Pham, Joan

 

An Assessment of CFD/CSD Prediction State-Of-The-Art Using the HART II International Workshop Data
Marilyn Smith and Byung-Young Min, Georgia Institute of Technology; Joon Lim, US Army AFDD (AMRDEC); Berend van der Wall, German Aerospace Center (DLR); James Baeder, University of Maryland; Robert Biedron and Doug Boyd, NASA Langley Research Center; Buvana Jayaraman, Science & Technology Corp. and Sung Jung, Konkuk University

 

An Assessment of Comprehensive Code Prediction State-Of-The-Art Using the HART II International Workshop Data
Berend van der Wall, German Aerospace Center (DLR); Joon W. Lim, US Army AFDD (AMRDEC); Marilyn Smith, Georgia Institute of Technology; Sung N. Jung, Konkuk University; Joëlle Bailly, Onera; James Baeder, University of Maryland; D. Douglas Boyd, Jr., NASA Langley

 

An Assessment of Current Methodology for Predicting Tiltrotor Blade-Vortex Interaction Aerodynamics
Bruce D. Charles, Ram D. Janakiram, Ahmed A. Hassan, McDonnell Douglas Helicopter Systems; Todd R. Quackenbush, Continuum Dynamics Incorporated

 

An Assessment of Empirical Models for Rotorcraft Ice Accretion
Jeewoong Kim, Lakshmi Sankar, and Stephen Marone (Georgia Institute of Technology) and Richard E. Kreeger (NASA Glenn Research Center)

 

An Assessment of Eurocopter Experience in HUMS Development and Support
Jean-Marc Pouradier, Eurocopter; Michel Trouvé, Eurocopter

 

An Assessment of Full Potential and Euler Solutions for Self-Generated Rotor Blade-Vortex Interactions
A.A. Hassan, McDonnell Douglas Helicopter Co., C. Tung, Aeroflightdynamics Directorate, U.S. Army AVSCOM, and L.N. Sankar, Georgia Institute of Technology

 

An Assessment of Full Potential and Euler Solutions for Self-Generated Rotor Blade-Vortex Interactions
Hassan, A.A., McDonnell Douglas Helicopter Company; Tung, C., AVSCOM; Sankar, L.N., Georgia Institute of Technology

 

An Assessment of RCAS Performance Prediction for Conventional and Advanced Rotor Configurations
Jimmy Ho, Science and Technology Corporation; Rohit Jain and Hyeonsoo Yeo and Mahendra Bhagwat, US Army

 

An Assessment of Real-Time Operating Systems for Use in Rotorcraft Mission Processing
Hamberg, Michael E.; Glusman, Brian J.; Turley, Kyle C.; DuBois, Thomas A.

 

An Assessment of Rotor Dynamics Correlation for Descending Flight Using CFD/CSD Coupled Analysis
Lim, Joon

 

An Assessment of the Impact of Technology on VTOL Weight Prediction
D.K. Unsworth and J. Sutton, Sikorsky Aircraft Division, United Technologies Corporation

 

An Assessment of the Long-Age Unsteady Rotor Hub Wake Physics for Empennage Analysis
David Reich and Sven Schmitz, The Pennsylvania State University; Rajiv Shenoy and Marilyn Smith, Georgia Institute of Technology

 

An Assessment of the State-of-the-art in Multidisciplinary Aeromechanical Analyses
Anubhav Datta, ELORET Corporation; Wayne Johnson, NASA Ames

 

An Assessment Of The State-Of-The-Art In The Design And Manufacturing Of Large Composite Structures For Aerospace Vehicles
Charles E. Harris, James H. Starnes, Jr., and Mark J. Shuart, NASA Langley

 

An Attack Helicopter Weapons Delivery Computer
J. A. Simpson, Norden Div., UAC

 

An Automated Approach for the Objective Evaluation of Practice Autorotations Using Available Aircraft Data
Nguyen, Phong; Pierce, Bradley; Walker, Joel

 

An Automated System Framework for Pre-Mission Success Evaluation of Medical Emergency Helicopters Operations – Critical Decision Acceptance Sub-Module
A. K. Sinha and R. Kusumo, Royal Melbourne Institute of Technology; P. Hogan and K. Laycock, Essendon Airport

 

An automatic anti-diffusion method for vortical flows based on Vorticity Confinement
M. Costes, ONERA and G. Kowani, DLR

 

An Autorotation Flight Director for Helicopter Training
Aponso, B.; Bachelder, E.

 

An Avionics Software Test and Evaluation Technique
T.B. Priest Jr. and B.P. Douglass, Bell Helicopter Textron

 

An Eagle Eye on Affordability, Bell's UAV Perspective
Robert J. Scholes, Bell Helicopter Textron, Inc.

 

An Economical Approach to Automated Flight Test Data Reduction
S. Walters, Aerospatiale Helicopter Corporation

 

An Effective Crashworthiness Design Optimization Methodology to Improve Helicopter Landing Gear Energy Absorption
Tho, Cheng-Ho; Wang, Bo Ping

 

An Efficient Computational Approach of Damage Tolerance Assessment for Helicopter Composite Components
Jeffery R. Schaff, Sikorsky Aircraft Corporation; Mark R. Gurvich, United Technologies; Endel V. Iarve, University of Dayton; David H. Mollenhauer, Air Force

 

An Efficient Kirchhoff Integration Method For Rotor Noise Prediction Starting Indifferently From Subsonically Or Supersonically Rotating Meshes
Rahier G. and Prieur J., ONERA

 

An Efficient Panel Ground Effect Model for Rotorcraft Simulations
Xin, Hong; He, Chengjian

 

An Efficient POD Based Technique to Model Rotor/Ship Airwake Interaction
Nischint Rajmohan, Jinggen Zhao and Chengjian He, Advanced Rotorcraft Technology Inc. and Jeewoong Kim, Lakshmi Sankar and J.V.R Prasad, Georgia Institute of Technology

 

An Electromagnetic Actuator For Individual Blade Control
David A. Fink, Diversified Technologies, Inc.; Timothy J. Hawkey, Diversified Technologies, Inc.; Marcel P.J. Gaudreau, Diversified Technologies, Inc.; Brent Wellman, Ames Research Center; Robert A. Ormiston, Ames Research Center

 

An Electronic Integrated Pilot Display Is Evaluated In North Sea Operations
R. J. van der Harten; Philip G. Cooper

 

An Embedded, Physics-Based Approach for Turboshaft Engine Continuous Power Assurance and Performance Monitoring
Goericke, Jan; Kouros, Areian; Moeckly, Kevin; Smith, Bert; Stramiello, Andrew

 

An Enhanced HUMS Foundation for Rotorcraft IVHM
Armenio, Christopher; Meyer, Theodore; Roemer, Michael; Schoeller, Michael

 

An Enhanced Integrated Aerodynamic Load/Dynamic Approach to Optimum Rotor Blade Design
A. Chattopadhyay, Analytical Services & Materials Inc. and Y.D. Chiu, Lockheed Engineering & Sciences Co.

 

An Enhanced Integrated Aerodynamic Load/Dynamic Approach to Optimum Rotor Blade Design
A. Chattopadhyay, Analytical Services & Materials Inc. and Y.D. Chiu, Lockheed Engineering & Sciences Co.

 

An Enhanced Method for Floquet Modal Identification
Hossein Saberi, Hong Xin, and Maryam Khoshlahjeh, Advanced Rotorcraft Technology, Inc.

 

An Entropy and Viscosity Corrected Potential Method for Rotor Performance Prediction
J . 0 . Bridgeman, Woodside Summit Group, R.C. Strawn and F.X. Caradonna, U.S. Army Aerof1ightdynamics Directorate

 

An Evaluation Methodology for Traffic Awareness Displays
De Maio, Joe; Dearing, Munro

 

An Evaluation of a Computer Code Based on Linear Acoustic Theory for Predicting Helicopter Main Rotor Noise
J. Davis, Sikorsky Aircraft Division, UTC, & T. Egolf, UTC Research Center

 

An Evaluation of a Navier-Stokes Code For Calculations of Retreating Blade Stall on a Helicopter Rotor
J.C. Narramore, Bell Helicopter Textron, L.N. Sankar, Georgia Institute of Technology, and R.E. Vermeland, CRAY Research, Inc.

 

An Evaluation of Active Control of Structural Response as a Means of Reducing Helicopter Vibration
A.E. Staple, Westland Helicopters Ltd.

 

An Evaluation of Advanced Rotorcraft Configurations for Emerging Military Applications
K. Wernicke & J. Fischer, Bell Helicopter Textron

 

An Evaluation of Anti-Icing Test Results for the AH-64D Apache Block III Engine Nose Gearbox Fairing
Buck, Laura; Dodson, Bob

 

An Evaluation of Coupled Rotor-Body Stability Using Reduced Order Linear Time Invariant (LTI) Models
Fahri Olcer, Georgia Institute of Technology; JVR Prasad, Georgia Institute of Technology

 

An Evaluation of Helicopter Autorotation Assist Concepts
A.H. Logan & R.D. Graves, Hughes Helicopters, Inc. and G.T. White, U.S. Army Applied Technology Laboratories

 

An Evaluation of High Order Spatial Accuracy Algorithms for Modeling Fixed and Rotary Wing Tip Regions
Nathan Hariharan, United Technologies Research Center; John Ekaterinaris, Nielsen Engineering and Research, Inc.; Yi Liu, Radhika Gupta, and L. N. Sankar, School of Aerospace Engineering

 

An Evaluation of the Influence of the Test Facility on Rotor Performance Characteristics
Cook, James; Smith, Marilyn

 

An Evaluation of the Proposed Specification for Handling Qualities of Military Rotorcraft, MIL-H-8501B, Utilizing Predicted and Actual SH-60B Handling Qualities
A.N. Cappetta and J.B. Johns, Naval Air Development Center

 

An Evaluation of the Residual Structural Integrity of a Helicopter Tail Rotor Shaft Subjected to a Ballistic Impact
Andrea Gilioli, Andrea Manes and Marco Giglio, Politecnico Di Milano

 

An Evaluation of the V22 Tiltrotor Aircraft With Variable Diameter Propeller Blades
David J. Kinney, NASA Ames; Mark H. Waters, ELORET Corp.

 

An Evaluation of Three Technologies for Rotating/Non-Rotating Data Transfer
Claude Matalanis and Nicholas Soldner and Sanjay Bajekal and Ulf Jonsson and Vijaya Lakamraju and Brian Wake, United Technologies Research Center; Jonathan Moore and Marcel Piet, DHI; Mark Scott, Sikorsky Aircraft

 

An Evaluation of Vertical Drag and Ground Effect Using the RSRA Rotor Balance System
R.J. Flemming, Sikorsky Aircraft Div., UTC and R.E. Erikson, NASA Ames Research Center

 

An Examination Of Engine Effects On Helicopter Aeromechanics
David M. O’Brien, Jr., Mark E. Calvert, and Steven L. Butler, U.S. Army RDECOM

 

An Examination of Rotor Loads due to On-Blade Active Controls for Performance Enhancement using CFD/CSD Analysis
R. Jain, HyPerComp Inc.; H. Yeo, Aeroflightdynamics Directorate, U.S. Army RDECOM; I. Chopra, University of Maryland

 

An Examination of Selected Problems in Rotor Blade Structural Mechanics and Dynamics Analysis
Hopkins, A.; Ormiston, Robert

 

An Examination of Selected Problems in Rotorcraft Aeroelastic Stability
A. Stewart Hopkins and Robert A. Ormiston, US Army

 

An Examination of Short Fatigue Crack Growth
R. L. Carlson and G. A. Kardomateas, Georgia Institute Of Technology

 

An Examination Of Some Rotor Aerodynamic Models Using The RSRA/X-Wing Model Test Data
S.J. Davis, J.P. Shanley and P. Buettiker, Sikorsky Aircraft Division, UTC

 

An Examination Of The Relations Between Rotor Vibratory Loads And Airframe Vibrations
Charles F. Niebanck, United Technologies Corporation

 

An Examination of Unsteady Airloads on a UH-60A Rotor: Computation Vs. Measurement
Robert Biedron and Elizabeth Lee-Rausch, NASA Langley Research Center

 

An Examination Of Vortex Convection Effects During Blade-Vortex Interaction
M.B. Homer, E. Saliveros, and R.A.McD. Galbraith, University of Glasgow

 

An Examination Of Vortex Convection Effects During Blade-Vortex Interaction
M.B. Homer, E. Saliveros, and R.A.McD. Galbraith, University of Glasgow

 

An Examination Of Vortex Convection Effects During Blade-Vortex Interaction
M.B. Horner, E. Saliveros, R.A. McD. Galbraith University of Glasgow

 

An Experiment to Simulate the Airloads and Wake Typical of a Hovering Rotor
Manikandan Ramasamy, Ames Research Center; Ashley Pete, Mahendra J. Bhagwat, Francis X. Caradonna, U.S. Army

 

An Experiment to Simulate the Airloads and Wake Typical of a Hovering Rotor
Manikandan Ramasamy, Ames Research Center; Ashley Pete, Mahendra J. Bhagwat, Francis X. Caradonna, U.S. Army

 

An Experimental and Analytical Investigation of Dynamic Stall Effects on Isolated Rotor Flap-Lag Stability
D. Barwey, G.H. Gaonkar, Florida Atlantic University and R.A. Ormiston, Aeroflightdynamics Directorate, U.S. Army AVSCOM

 

An Experimental and Analytical Investigation of Dynamic Stall Effects on Isolated Rotor Flap-Lag Stability
D. Barwey, G.H. Gaonkar, Florida Atlantic University and R.A. Ormiston, Aeroflightdynamics Directorate, U.S. Army AVSCOM

 

An Experimental and Analytical Investigation of Scissors Rotor Aerodynamics in Hover
Xu, Guo-Hua

 

An Experimental And Analytical Investigation On The Response Of Gr/Ep Composite I-Frames
E. Moas, Jr., Analytical Services and Materials, Inc.; R.L. Boitnott, U.S. Army; O.H. Griffin, Jr., Virginia Polytechnic Institute and State University

 

An Experimental and Analytical Study of the Influence of Aerodynamic Design Parameters on the Static Performance of Ducted Fans for Tail Rotor Applications
Jack E. Fairchild, Robert L. Stewart, and N. N. Batra, University of Texas at Arlington

 

An Experimental Comparison of Transmission Vibration Responses from OH-58 and AH-1 Helicopters
Edward M. Huff, NASA Ames Research Center; Irem Y. Tumer, NASA Ames Research Center; Marianne Mosher, NASA Ames Research Center

 

An Experimental Evaluation of Generalized Predictive Control for Tiltrotor Aeroelastic Stability Augmentation in Airplane Mode of Flight
Raymond G. Kvaternik, NASA Langley Research Center; David J. Piatak, NASA Langley Research Center; Mark W. Nixon, NASA Langley Research Center; Chester W. Langston, NASA Langley Research Center; Jeffrey D. Singleton, NASA Langley Research Center; Richard L. Bennett, Bell Helicopter Textron; Ross K. Brown, Bell Helicopter Textron

 

An Experimental Evaluation of Wind Tunnel Wall Correction Methods for Helicopter Preformance
H.J. Langer, Institut fur Flugmechanik, R.L. Peterson, NASA Ames Research Center, and T.H. Maier, U.S.Army AATD

 

An Experimental Investigation of a Bearingless Model Rotor in Hover
S. Dawson, U.S. Army Research and Technology Laboratories

 

An Experimental Investigation of a Quad Tilt Rotor in Low Speed Forward Flight
A. Radhakrishnan, Univ. of Maryland, et al.

 

An Experimental Investigation of STOL Lateral-Directional Flying Qualities and Roll Control Power Requirements Using the Variable-Stability X -22A Aircraft
J. V. Lebacqz and R. C. Radford, Calspan Corp., and R. E. Smith, NRC, Canada.

 

An Experimental Investigation of STOL Longitudinal Flying Qualities in the Landing Approach Using the Variable Stability X-22A Aircraft
J. M. Schuler, R. E. Smith, J. V. Lebacqz, Cornell Aeronautical Laboratory, Inc.

 

An Experimental Method for Water Droplet Impingement Measurement
Michael B. Bragg, Michael Cebrzynski and Jonathan Reichhold, University of Illinois; Dave Sweet, Tom Waples, and Rob Shick, BFGoodrich Aerospace

 

An Experimental Method for Water Droplet Impingement Measurement
Michael B. Bragg, Michael Cebrzynski and Jonathan Reichhold, University of Illinois; Dave Sweet, Tom Waples, and Rob Shick, BFGoodrich Aerospace

 

An Experimental Study of Main Rotor/Tail Rotor/Airframe Interaction in Hover
D.T. Balch, Sikorsky Aircraft Division, UTC

 

An Experimental Study of Rotorcraft in Ground Effect
G. McCauley, W. Tsai, O. Savas, University of California Berkeley

 

An Experimental Study Of Techniques For Increasing The Lead-Lag Damping Of Soft Inplane Hingeless Rotors
W. G. Bousman; D. L. Sharpe; R. A. Ormiston

 

An Exploration of Discontinuous Time Synchronous Averaging Using Helicopter Flight Vibration Data
Admin, Mira; Huff, Edward

 

An Exploration of the Physics of Dynamic Stall
V. Raghav, P. Richards, N. Komerath, M. Smith, Georgia Institute of Technology

 

An Exploratory Aerodynamics Limits Test with Analytical Correlation
M. Floros, N. Gold, Raytheon ITSS; W. Johnson, NASA Ames

 

An Exploratory Investigation of the Effects of Large Variations in Rotor Systems Dynamics Design Parameters on Helicopter Handling Characteristics in NOE Flight
R.T.N. Chen and P.D. Talbot

 

An H-Infinity Technique for Improved Higher Harmonic Control
Frank Fan and Steven R. Hall, Massachusetts Institute of Technology

 

An Implicit Floquet Analysis for Rotorcraft Stability Evaluation
Olivier A. Bauchau, Georgia Institute of Technology; Yuri G. Nikishkov, Georgia Institute of Technology

 

An Improved Concept for a Crashworthy Cyclic Control Stick
Brian L. Carnell, SURVICE Engineering Company; James C. Garman, Sikorsky Aircraft Corporation

 

An Improved Dynamic Stall Model for Rotor Airfoil Based on Experimental Investigations
Wang Qing, Zhao Qi-jun, Zhao Guo-qing, Nanjing University of Aeronautics and Astronautics

 

An Improved QFD Method for Common Avionics System Demands Analysis
Ming Zhu, Lei Zhang, Jingjing Song and Zhe Wu, Beijing University of Aeronautics and Astronautics

 

An Impulse Response Driven Approach for Optimizing Bearing Enveloping Diagnostics
Matthew Szelistowski and Steve Shepard and Daniel Wade, Aviation Engineering Directorate

 

An In-Flight Investigation of Symbology Drive Law Improvements to an Operational Attack Helicopter
J.A. Schroeder, W.S. Hindson, NASA Ames Research Center, and M.M. Eshow, Aeroflightdynamics Directorate, U.S. Army AVSCOM

 

An In-Flight Investigation of Symbology Drive Law Improvements to an Operational Attack Helicopter
Jeffery A. Schroeder, NASA Ames; Michelle M. Eshow, U.S. Army ASC; William S. Hindson, NASA Ames

 

An Innovative Approach to Supplier Cost Control
J.M. Rosen, Sikorsky Aircraft Division, UTC

 

An Innovative Technique for Static and Dynamic V/STOL Testing
Lewis, Ernest L., Naval Air Systems Command; Culpepper, Richard G., NASA; Hancock, Virgil R., Rockwell International Corporation

 

An Integrated Airloads-Inflow Model for Use in Rotor Aeroelasticity and Control Analysis
D.A. Peters and A. Su, Georgia Institute of Technology

 

An Integrated Analysis Code with CFD/Rotor Dynamics Coupling Developed in JAXA
Yasutada Tanabe and Shigeru Saito, Japan Aerospace Exploration Agency (JAXA)

 

An Integrated Approach for Gear Health Prognostics
David He and Jinghua Ma, University of Illinois-Chicago; Eric Bechhoefer, NRG Systems; and Paula Dempsey, NASA Glenn Research Center

 

An Integrated Approach to Rotorcraft Total Survivability and Operational Durability
Jeffery Schaff, Sikorsky Aircraft Corp, Mark Robeson, Army AATD

 

An Integrated Design Environment for NDARC
Jeffrey D. Sinsay (US Army Aviation Development Directorate - AFDD), David M. Hadka, and Sara E. Lego (Pennsylvania State University)

 

An Integrated Display Concept For Helicopters And Vtol Aircraft*
Theodor A. Dukes

 

An Integrated Framework for Adaptive Optimal Obstacle Avoidance for Rotary-Wing UAVs
Keeryun Kang, J.V.R. Prasad and Eric Johnson, Georgia Institute of Technology

 

An Integrated Health and Usage Monitoring System for the SH-60B Helicopter
G. P. Cleveland and C. Trammel, Smiths Industries Aerospace

 

An Integrated Hydraulic Control System Combining Boost, Control Fuel, Stability Augmentation, and Gust Alleviation
R. P. Carroll, C. J. Wirth, and F. L. Smith, Kaman Aircraft Corp.

 

An Integrated Rotorcraft Damage Tolerance Methodology for Design, Analysis, and Qualification of Fatigue Critical Metal Airframe Structure
Preston R. Bates, Michael Urban, and James Cycon, Sikorsky Aircraft Corporation

 

An Integrated Simulation Environment as a Strategy in Rotorcraft UAVs Preliminary Design
Marzio Luigi Preatoni, AGUSTA; Roberto Pretolani, Gian Marco Saggiani, and Barbara Teodorani, University of Bologna

 

An Integrated System of Airborne and Ground-Based Instrumentation for Flying Qualities Research With the X-22 Airplane
J. L. Beilman, Cornell Aeronautical Laboratory

 

An Integrated Three Dimensional Audio Display For The Rotorcraft Pilot's Associate
Reid Benes, The Boeing Company

 

An Integrated Vehicle Health Management System For Next Generation CBM
Michael Schoeller, Theodore S. Myers, Jeffery Hoffman, and Michael Roemer, Impact Technologies, LLC; Jason Fetty and Treven Baker, US Army (RDECOM)

 

An Integrated, Physics Based, Lubrication Analysis Methodology for Helicopter Transmission Gear Surfaces with Asperities
Carmen Cioc, The University of Toledo; Laurentiu Moraru, The University of Toledo; Theo Keith, The University of Toledo; Ahmet Kahraman, The University of Toledo

 

An Integrated, Real-Time Oil Quality Monitor and Debris Measurement Capability for Drivetrain and Engine Systems
Argenna, Garrett; Byington, Carl; Goddard, Kevin; Mackos, Nicholos; Moffatt, John; Moss, Rachel; Palmer, Carl; Toms, Allison; Ture, Cody

 

An Integration Approach For Rotorcraft Pilot's Associates
C.F. Doty, Boeing Helicopters

 

An Intelligent Approach to Coordinated Control of Multiple Unmanned Aerial Vehicles
Tang, Liang; Vachtsevanos, George; Reimann, Johan

 

An Interference-Free Quad-Tilt Design
Hurley, F. X.

 

An Interview with Colonel Floyd Harold "Hal" Kushner, M.D., F.A.C.S U.S. ARMY Flight Surgeon and Vietnam Prisoner of War
Paul Fardink, U.S. ARMY (Retired)

 

An Interview with Major General Patrick H. Brady, Dust Off Innovator and Medal of Honor Recipient
Paul Fardink, U.S. ARMY

 

An Interview with the Father of Army Aviation LTG Robert R. Williams, USMA '40
Fardink, Paul

 

An Interview with the First Branch Chief of Army Aviation Major General Carl H. McNair, Jr., USMA '55
Lieutenant Colonel Paul Fardink, U.S. Army (Retired)

 

An Inverse Aerodynamic Design Method for Rotor Blades in Forward Flight
Fidencio Tapia, Lakshmi N. Sankar, and Daniel P. Schrage, Georgia Institute of Technology

 

An Investigation into the Aerodynamics of Trailing Edge Flaps with Overhang and Gap
Arun I. Jose, Asitav Mishra, James D. Baeder, University of Maryland

 

An Investigation into the Effects of Body-borne Equipment on Occupant Injury Under Simulated Vertical Impact with Seat 'Bottom-out'
Daniel Aggromito and Bernard Chen and Wenyi Yan, Monash University; John Wang, Defence Science and Technology Organisation; Rodney Thomson, Cooperative Research Centre for Advanced Composite Structures

 

An Investigation of Aerodynamic Interactions between a Rotor and a Fuselage in Forward Flight
J.G. Leishman, N. Bi, D.K. Samek and M. Green, University of Maryland

 

An Investigation of Excessive Blade Flapping in the Robinson R-22 Helicopter
S. Sarathy, Clark Atlanta University; D. Schrage and P. Losier, Georgia Institute of Technology

 

An Investigation of Flutter in Very Large Wind Turbine Blade Designs
Brian Owens and D. Todd Griffith and Brian Resor, Sandia National Laboratories, John Hurtado, Texas A&M Universitry

 

An Investigation of Heavy Lift Helicopter Display Problems
A. T. Sherbert, Jr., Boeing/Vertol

 

An Investigation of Helicopter Rotor Blade Flap Vibratory Loads
W.G. Bousman and T.H. Maier, NASA Ames Research Center

 

An Investigation of Large Tilt-Rotor Hover and Low Speed Handling Qualities
Carlos Malpica, NASA Ames Research Center; William Decker, NASA Ames Research Center; Colin Theodore, NASA Ames Research Center; Ben Lawrence, San Jose State University Research Foundation; James Lindsey, Monterey Technologies; Chris Blanken, U.S. Army Aeroflightdynamics Directorate

 

An Investigation of Large Tilt-Rotor Short-Term Attitude Response Handling Qualities Requirements in Hover
Berger, Tom; Blanken, Chris; Decker, William; Malpica, Carlos; Theodore, Colin

 

An Investigation of Single-Piloted Advanced Cockpit and Control Configurations for Nap-of-the-Earth Helicopter Combat Mission Tasks
L.A. Haworth, C.C. Bivens and R.J. Shively, U.S. Army Aeroflightdynamics Directorate

 

An Investigation of Soft-Inplane Tiltrotor Aeromechanics Using Two Multibody Analyses
P. Masarati, Politecnico di Milano ; D. Piatak, NASA LaRC; J. Singleton, US Army VTD; P. Mantegazza, Politecnico di Milano

 

An Investigation of Soft-Inplane Tiltrotor Aeromechanics Using Two Multibody Analyses
Jeffrey D. Singleton, NASA; Pierangleo Masarati, Paolo Mantegazza, Politecnico di Milano; David J. Piatak, NASA; Jeffrey D. Singleton, Mark W. Nixon, Army

 

An Investigation of the Aerodynamics of an RAE Swept Tip Using A Model Rotor
P. G. Wilby, RAE and J. J. Philippe, ONERA

 

An Investigation of the Expectation Maximization Technique for an Unsupervised Machine Learning Application of Rotorcraft HUMS Data
Lance Antolick, RMCI, Inc.

 

An Investigation of the Flow Field and Drag of Helicopter Fuselage Configurations
James Gillespie, USAAMR&DL, Ft. Eustis, Va.

 

An Investigation Of The Impact Of Automatic Flight Control System Saturation On Handling Qualities In Hover/Low Speed Manoeuvres
J. Howitt, Defence Evaluation & Research Agency; M. S. Whalley, NASA Ames Research Center; Dr. M. E. Strange, Defence Evaluation & Research Agency; Dr. G. J. W. Dudgeon, Defence Evaluation & Research Agency

 

An Investigation of the Mechanical Airloads Problem for Evaluating Rotor Blade Structural Dynamics Analysis
R. Ormiston, US Army AFDD

 

An Investigation of the Numerical Prediction of Static and Dynamic Stall
Shelton, Andrew; Abras, Jennifer; Hathaway, Brandon; Sanchez-Rocha, Martin; Smith, Marilyn J.; Menon, Suresh

 

An Investigation Of The Trailing Vortex System Generated By A Jet-Flapped Wing Operating At High Wing Lift Coefficients
William J. Schumacher, U.S. Army

 

An Investigation of the Vibratory and Acoustic Benefits Obtainable by the Elimination of the Blade Tip Vortex
Richard P. White, Jr., RASA, Inc. (Standby)

 

An Investigation of the Wave Bearing Attenuation Effects on Vibration and Noise Generated by a Gearbox Compared to the Rolling Element Bearings
Florin Dimofte, The University of Toledo; Nicoleta Ene, The University of Toledo; Fred Oswald, NASA GRC

 

An Investigation of Variable Rotor RPM on Performance and Trim
Gandhi, Farhan; Steiner, Jason; Yoshizaki, Yuji

 

An Investigation of VTOL Operational Problems Due to Downwash Effects
Richard R. Pruyn and Leonard Goland

 

An Investigation of Wake Curvature Dynamics for Helicopter Maneuvering Flight Simulation
Peters, D.; Prasad, J.; Zhao, J.

 

An NDT Assessment of the V-22 Osprey
T.G. Marshall, Bell Helicopter Textron, Inc.

 

An Obstacle Alerting System for Agricultural Application
De Maio, Joe

 

An Open System Architecture Approach to Providing CNS/ATM Compliant Solutions for Helicopters
Civilikas, Robert G.

 

An Operationally-Applicable Objective Method For The Analysis And Evaluation Of The Flights Of Helicopter Mission Task Elements During Field-Of-View Trials
Kenneth L Edwards, John W Buckle, Mark J Doherty, Lionel J Lee, Adam C Pratty, John F White, Defence Evaluation and Research Agency

 

An Operator's Viewpoint of Helicopter Safety
J. C. Weadock

 

An Overview of H-60 A2L Remanufacturing
Richard Allard, Jr., Sikorsky Aircraft

 

An Overview of MH2000, Development and Flight Tests
Kiyoshi Sakura, Mitsubishi Heavy Industries, Ltd.

 

An Overview of Possible and Not-so-Possible Tasks for Active Control of Sound and Vibration
Andreas H. von Flotow, Massachusetts Institute of Technology

 

An Overview of Possible and Not-so-Possible Tasks for Active Control of Sound and Vibration
Andreas H. von Flotow, Massachusetts Institute of Technology

 

An Overview of Possible and Not-so-Possible Tasks for Active Control of Sound and Vibration
Andreas H. von Flotow, Massachusetts Institute of Technology

 

An Overview of Rotary Wing Ship Suitability Testing at NAVAIR
Chris Szymendera, NAVAIR

 

An Overview of Rotor Noise in Maneuvering Flight
Hsuan-nien Chen and Kenneth S. Brentner, The Pennsylvania State University

 

An Overview of SHOL Testing Within The Royal Netherlands Navy
Captain Alrik Hoencamp, MSc, NLDA

 

An Overview of the AH-64D Apache Block III Engine Nose Gearbox Fairing Icing Wind Tunnel Test
Adams, Nathan; Buck, Laura; Higman, Jerry; Rodriguez, Nicolas; Wiersma, Henry

 

An Overview of the RQ-8A Fire Scout VTUAV Ground Resonance Stability Validation Program
R.B. Walden, Naval Air Systems Command; R. Common, Northrop Grumman Corporation; H. Hoefferle, Schweizer Aircraft Corporation,

 

An Overview of the US/UK ASTOVL Programs, 1983-1994
David C. Aronstein, Ph.D., Michael J. Hirschberg, ANSER, Inc.

 

An overview on Practical Application of Helicopter Noise Certification rules
Mr. Estival and F. d'Ambra, Aerospatiale — Helicopter Division

 

An Unmanned Cargo-Delivery System for Rotorcraft Landing to Unprepared Sites
 James Paduano and John Wissler and Graham Drozeski and Michael Piedmonte and Navid Dadkhah and Jim Francis and Charles Shortlidge and Jason Bold and Fritz Langford and Mark Chaoui and Cheng-Jen Liu and Eric Foster, Aurora Flight Sciences; Sanjiv Singh and Lyle Chamberlain and Brad Hamner and Hugh Cover and Adam Stambler and Ayman Singh and Samuel Nalbone and Marcel Bergerman, Near Earth Autonomy; Sebastian Scherer and Sanjiban Choudhury and Silvio Maeta and Sankalp Arora and Daniel Maturana, Carnegie Mellon University; Cindy Dominguez and Brian Moon and Robert Strouse and Lisa Papautsky, Applied Research Associates, Inc.; David Mindell, Massachusetts Institute of Technology; Dino Cerchie and Bryan Chu and Jason Graham and Christine Cameron and Mark Hardesty and Roger Hehr, The Boeing Company; Doug Limbaugh and James Bona and David Barnhard and Desare'a Chessar, Kutta Technologies, Inc.

 

An Unmanned Helicopter Vehicle System Development
Fei-Bin Hsiao, Hian-Kun Tenn, Shau-Shiun Jan, Fu-Yuen Hsiao, Jyh-Ching Juang, Ying-Chih Lai, Weoi-Leong Chan, Sheng-Yen Hsieh, Chun-Chih Chen, Li-Che Tseng, National Cheng Kung University

 

An Unmanned Helicopter Vehicle System Development
Fei-Bin Hsiao, Hian-Kun Tenn, Shau-Shiun Jan, Fu-Yuen Hsiao, Jyh-Ching Juang, Ying-Chih Lai, Weoi-Leong Chan, Sheng-Yen Hsieh, Chun-Chih Chen, Li-Che Tseng, National Cheng Kung University

 

An Unsteady Airload Model with Dynamic Stall for Rotorcraft Simulation
Dr. Cheng-Jian, Dr. Ronald W. Du Val, Advanced Rotorcraft Technologies, Inc.

 

An Unsteady Ducted Fan Model for Rotorcraft Flight Simulation
C. He, H. Xin, Advanced Rotorcraft Technology, Inc.

 

An Unstructured-Adaptive Cartesian CFD Method for Hover Prediction
Mavriplis, Dimitri; Potsdam, Mark; Sankaran, Venkataswaran; Sitaraman, Jay; Wissink, Andrew; Yang, Zhi

 

An Update Status for the SH-60 Helicopter Integrated Diagnostic System (HIDS) Program - Diagnostic and Prognostic Experience
Bill Hardman, Naval Air Warfare Center Aircraft Division; Andrew Hess, Naval Air Warfare Center Aircraft Division; Mike McGonigle, Naval Air Warfare Center Aircraft Division; Jon Sheaffer, Naval Air Warfare Center Aircraft Division

 

AN/ASN-86 Inertial Navigation Set
R. Creed, USA Electronics Command, and J. B. Hughes, Guidance & Control Div., Litton Industries

 

Analysis and Ballistic Testing of Three Similar Rotorcraft Structures Against the 23mm HEI Threat
C.E. Sparks, M.A. Gonzalez, C.A. Kubes, Bell Helicopter Textron, Inc..

 

Analysis and Control of A Magnetorheological Landing Gear System For a Helicopter
Young-Tai Choi, Ryan Robinson, Wei Hu, and Norman M. Wereley, University of Maryland; Terence S. Birchette and Akif Bolukbasi, The Boeing Co. and Jin Woodhouse, U.S. Army AATD

 

Analysis And Control Of The Transient Shipboard Engagement Behavior Of Rotor Systems
Jonathan A. Keller, The Pennsylvania State University; Edward C. Smith, The Pennsylvania State University

 

Analysis And Design Of Dynamically Loaded Fittings
Rodney H. Jones, J. Donn Hethcock, and B.R. Mullins, Bell Helicopter Textron, Inc.

 

Analysis and Design of Tow-Steered Variable Stiffness Composite Laminates
Brian F. Tatting, ADOPTECH, Inc.; Zafer Gürdal, Virginia Tech

 

Analysis and Development of Impact Resistant Light Weight Composite Aircraft Structure
D.K. McCarthy, R. LaHaie, R. Gaddy, The Boeing Company

 

Analysis and Reconstruction of Helicopter Load Spectra
A.K. Khosrovaneh and N.E. Dowling, Virginia Polytechnic Institute and State University

 

Analysis and Simulation of Piloted Performance in Crane-Type Helicopters in Hover
R. T. Lytwyn and F. White, Boeing Vertol Co., and R. P. Smith, USAAMRDL, Eustis.

 

Analysis and Synthesis of Highly Flexible Helicopter Drivelines with Flexible Matrix Composite Shafting
Mayrides, Bryan; Smith, Edward C.; Wang, K.W.

 

Analysis and Testing of a Model-Scale Magnetorheological Fluid Helicopter Lag Mode Damper
Gopalakrishna M. Kamath, Norman M. Wereley, University of Maryland; Mark R. Jolly, Lord Corporation

 

Analysis and Testing of Fiber-Reinforced Thermoplastoc Composite Vertical Stabilizer Skins for an Advanced Attack Helicopter
A. Kaizoji, McDonnell Douglas Helicopter Co.

 

Analysis and Testing of the Bell Model 525 Helicopter Flight Control System

 

Analysis Methods to Control Performance Variability and Costs in Aircraft Turbine Engine Manufacturing
K. E. Sheldon, Virginia Polytechnic Institute and State University; C. M. Anderson-Cook, Virginia Polytechnic Institute and State University; W.F. O?Brien, Virginia Polytechnic Institute and State University

 

Analysis of a Helicopter Tail Landing Gear System Featuring Electrorheological Fluids
Choi, Y.; Wereley, N.

 

Analysis of a Hovering Rotor in Icing Conditions
Kreeger, Richard; Narducci, Robert

 

Analysis Of A Laminated Blade Retention System
Robert T. Fort and Dennis K. McCarthy, McDonnell Douglas Helicopter Systems

 

Analysis of a Multi-Flap Rotor System for Swashplateless Rotor Control
Martin Sekula, NASA Langley Research Center; Matthew Wilbur, ARLVTD

 

Analysis of a Multi-Flap Rotor System for Swashplateless Rotor Control
Martin Sekula, NASA Langley Research Center; Matthew Wilbur, ARLVTD

 

Analysis of a Ramp Roller Clutch System
Liu, Lin; Strickland, Douglas

 

Analysis of Aeroelastic Rotors using Hybrid-CFD Techniques
Nicolas Reveles, Marilyn Smith, Georgia Institute of Technology

 

Analysis of Aeroelastic Rotors using Hybrid-CFD Techniques
Nicolas Reveles, Marilyn Smith, Georgia Institute of Technology

 

Analysis of Bearingless Main Rotor Dynamics with the Inclusion of an Improved Time Domain Nonlinear Elastomeric Damper Model
Farhan Gandhi and Inderjit Chopra, University of Maryland

 

Analysis of Causes and Countermeasures of Helicopter Accident from the Engineering Viewpoint
Myeang-Hyen Bae, Yeon-Bok Chu, Duck-Joo Lee, KAIST

 

Analysis of CFD Modeling Techniques Over the MV-22 Tiltrotor
Abras, Jennifer; Narducci, Robert

 

Analysis Of Complex Rotor-Airframe Coupled Instabilities By Energy Flow Considerations
Oliver Oberinger and Manfred Hajek, TU München

 

Analysis Of Complex Rotor-Airframe Coupled Instabilities By Energy Flow Considerations
Oliver Oberinger and Manfred Hajek, TU München

 

Analysis of Crash Resistant Fuel Systems and Airframe Structure Interaction in a Crash Environment
A.O. Bolukbasi, McDonnell Douglas Helicopter Co.

 

Analysis of Dynamic Characteristics of Asymmetric Bifilar Pendulum Absorber
SI Ying-zhan, GAO Ya-dong, WANG Hua-ming, Nanjing University of Aeronautics & Astronautics

 

Analysis of Dynamic Response of Direction Control for Semi-Differential Co-Axial Helicopter
Ming Chen, Ji-zhong Hu, Beijing University of Aeronautics and Astronautics

 

Analysis of Dynamic Rig Test Data for an Axial/Centrifugal Compressor Operating at Design Speed
A. Karl Owen, George A. Bobula, ARL Vehicle Propulsion Directorate, NASA Lewis

 

Analysis of Energy-Absorbing Seat Configurations
K.L. Winkelman and D.H. Laananen, Arizona State University

 

Analysis of Flapped Rotors Using CFD and Indicial Methods
Gagliardi, A.; Beedy, J.; Steijl, R.; Barakos, G.; Badcock, K.

 

Analysis of Handling Qualities Design Criteria for Active Inceptor Force-Feel Characteristics
Carlos Malpica, NASA Ames Research Center, Jeff Lusardi, U.S. Army RDECOM

 

Analysis of Health and Usage Monitoring System (HUMS) Users Perspective towards Mission Benefits Using Regression Analysis
Tanzina Zaman and Abdel E. Bayoumi, University of South Carolina

 

Analysis of Helicopter Air-to-Air Combat Tests, Design Implications
Kenneth B. Amer, RAND Corporation

 

Analysis of Helicopter Flight Dynamics Through Modeling and Simulation of Primary Flight Control Actuation System
Hunter Nelson and Roberto Celi, University of Maryland

 

Analysis of Helicopter Stability Augmentation Obtainable with the Oehmichen Pitch-Flap Coupling Concept
G. Bruning

 

Analysis of Helicopter/Ship Aerodynamic Interactions
O.A.F. Mello, J.V.R. Prasad, L.N. Sankar, Georgia Institute of Technology; W. Tseng, Naval Air Warfare Center

 

Analysis of High Resolution Unsteady Airloads for Helicopter Rotor Blades
Todd R. Quackenbush, C-M G. Lam, D.A. Wachpress, Continuum Dynamics, D.B. Bliss, Duke University.

 

Analysis of Hydrodynamic Ram Compliant Structure
Dennis K. McCarthy, Boeing; Dr. Mark E. Robeson, US Army

 

Analysis of Impact Behavior of Thick Rotorcraft Composite Components: Approach and Implementation
Brian Bouquillon and Mark Davis, Sikorsky Aircraft Corporation; Mark Gurvich and Prabhakar Rao and Patrick Clavette, United Technologies Research Center

 

Analysis of Interlaminar Damages in Thick Rotorcraft Composite Components by Embedded Sensors
Bordick, Nate; Butler, Shaoluo; Ghoshal, Anindya; Gurvich, Mark; Urban, Michael; Welsh, Gregory

 

Analysis of Lag Motion Damping for Upgraded Mil-24 Main Rotor Blade in Hover, Level and Maneuvering Flight Based on Flight Test Results
Valery Ivchin, Mil Moscow Helicopter Plant

 

Analysis of Large Civil Tilt Rotor Wind Tunnel Blockage and Validation Using RotCFD
S. Esma Sahin (Science & Technology Corp), Carl Russell (NASA Ames Research Center), Eduardo Solis (Monterey Technologies), and R. Ganesh Rajagopalan (Iowa State University)

 

Analysis Of Leading Edge Deformation For Dynamic Stall Prevention
James G. Reuster and James D. Baeder, University of Maryland

 

Analysis of Magnetic Communications for Use on Rotorcraft
Sanjay Bajekal, Vijay Lakamraju and Nicholas Soldner, United Technologies Research Center

 

Analysis of Measured and Predicted Acoustics from an XV-15 Flight Test
D. Douglas Boyd, Jr., NASA Langley Research Center; Casey L. Burley, NASA Langley Research Center

 

Analysis Of Mixed Critical Avionics And Systems
Brian LaValley, blavallley@wwtechgroup.com, Chris Walter, WW Technology Group

 

Analysis of Model Uncertainties Using Inverse Simulation
Steffen Greiser and Wolfgang von Grünhagen, DLR (German Aerospace Center)

 

Analysis of Navigation Requirements for Commercial VTOL Operations
William C. Hoffman and John Zvara, Aerospace Systems Inc., and Walter M. Hollister, MIT

 

Analysis Of Potential Helicopter Vibration Reduction Concepts
Anton J. Landgrebe and Mark W. Davis, United Technologies Research Center

 

Analysis of Quasi-Unbalanced Structures Exhibiting Intrinsically Smart Behavior
M. Garfinkle, Philadelphia University; C. Pastore, Philadelphia University; A. Bogdanovich, 3Tex, Inc.; S. Greenhalgh, Prodesco, Inc.

 

Analysis of Real-Time Rotor Stall Detection Methods
Grill, Ivan; Kim, Seong-Joo; Prasad, J.V.R.; Vachtsevanos, George

 

Analysis of Rotor Airloads Based on CFD/CA Loose Coupling
Xiao Yu, Xu Guo-Hua, Shi Yong-Jie, Nanjing University of Aeronautics and Astronautics

 

Analysis of Rotor Blade Dynamics Using Experimental UH-60A Airloads Obtained at the DNW
M.S. Torok and R.K. Goodman, Sikorsky Aircraft

 

Analysis of Rotorcraft Aerodynamics/Acoustics During Coordinate Turns of Research Helicopter
Choongmo Yang, Takashi Aoyama, Hirokazu Ishii and Yoshinori Okuno, Japan Aerospace Exploration Agency (JAXA) 

 

Analysis of Start-up and Shutdown of Rotor in Complex Wind Conditions on Sea-Based Oil Rig
Jianhua Zhang, Edward C. Smith, Frank Zajaczkowski, The Pennsylvania State University

 

Analysis of Start-up and Shutdown of Rotor in Complex Wind Conditions on Sea-Based Oil Rig
Jianhua Zhang, Edward C. Smith, Frank Zajaczkowski, The Pennsylvania State University

 

Analysis of the Aerodynamically Deployable Wings of the Mono Tiltrotor
Leishman, Gordon; Samsock, John

 

Analysis of the Diving Turn Maneuver for the UH-60A Rotor
Ritu Marpu and Lakshmi Sankar, Georgia Institute of Technology

 

Analysis of the Diving Turn Maneuver for the UH-60A Rotor
Ritu Marpu and Lakshmi Sankar, Georgia Institute of Technology

 

Analysis of the Effectiveness of Wire Strike Protection on Army Helicopters
LeRoy T. Burrows, U.S. Army AATD (ATCOM)

 

Analysis of the VC2 Vorticity Confinement Scheme
M. Costes, ONERA

 

Analysis of Trailing-Edge Flap Control for Minimum Vibrations Using CFD/CSD Analysis

Brian E. Wake, C. Aaron Reimann and Milos Ilak, United Technologies Research Center; Stephen M. Makinen and Jinsong Bao, Sikorsky Aircraft Corporation

 

Analysis of U.S. Civil Rotorcraft Accidents Caused by Vehicle Failure or Malfunction, 1998 - 2004
Liu, Lin; Pines, Darryll. J.

 

Analysis of US Civil Rotorcraft Accidents from 1990 to 1996 and Implications for a Safety Program
Laura Iseler, NASA Ames Research Center; Joe De Maio, Ames Research Center

 

Analysis of V-22 Rotor Blade Performance Enhancements for Improved Payload
Bridgeman, John; Cummings, Antonette; Kisor, Ron; Narramore, Jimmy

 

Analysis of V-22 Tilt-Rotor Aircraft Using Panel Methods
G.J. Carlin, Jr., W.E. Staedeli and R.M. Hodges, Jr., Boeing Vertol Co

 

Analysis of Vertical Axis Wind Turbine Aerodynamics by Using a Multi-Fidelity Approach
Yi Han and Jayanarayanan Sitaraman, University of Wyoming; Yong Dan, Northwest University (China)

 

Analysis of Vorticity Confinement for Compressible Flows
Costes, M.; COSTES, Michel

 

Analysis of VTOL Transition Dynamics
D. L. Key, Cornell Aeronautical Laboratory, Inc.

 

Analysis on Aerodynamic and Acoustic Characteristics for Scissors Tail-Rotors in Forward Flight
Fan Feng, Shi Yong-Jie, Xu Guo-Hua, Ye Zhou, Nanjing University of Aeronautics and Astronautics

 

Analysis Refinements for Prediction of Rotor Vibratory Loads in High-Speed Forward Flight
Datta, Anubhav; Sitaraman, Jayanarayanan; Baeder, James D.; Chopra, Inderjit

 

Analysis The Different Rotational Velocity Impact On Eccentric Vortex Inside Of The Fanwing
Wu Hao-dong, Tang Zheng-fei, Tang Min, Science and Technology on Rotorcraft Aeromechanics Laboratory

 

Analysis, Design, & Optimization of the Helicopter Active Control Technology (HACT) Flight Control System
Johnson, Christopher K.; Tischler, Mark B.; Mittleider, David; Cheung, Kenny K.

 

Analysis, Design, and Testing of Fuselage Tuning for the CH-47 Chinook
Tom Rosenberger, The Boeing Company; Krishan Ahuja, The Boeing Company; CW4 Randy Wells, U.S. Army ATTC

 

Analysis, Modeling and Simulation: The Front End of the Systems Engineering Process
Kraay, Anthony; Macpherson, Dale

 

Analysis, Modeling and Simulation: The Front End of the Systems Engineering Process
Dale Macpherson and Tony Kraay, The Boeing Company

 

Analytic and Experimental Verification of the NOTAR Circulation Control Tail Boom
K.M. Morger, Hughes Helicopters, Inc. and D.R. Clark, Analytical Methods, Inc.

 

Analytic Insight into the Structural Couplings and Nonlinear Formulation of Solid and Thin-Walled Composite Blades
O. Rand and S. Barkai, Technion - Israel Institute of Technology

 

Analytic Investigation of Advancing Blade Drag Reduction by Tip Modifications
Tauber, Michael E., NASA

 

Analytical & Experimental Investigation Of V-Type Empennage Contribution To Directional Control In Hover & Forward Flight

C.E. Freeman & W.T. Yeager, US Army RTL, Langley

 

Analytical and Experimental Micro Rotorcraft Design Studies
Todd R. Quackenbush, Daniel A. Wachspress, Alexander H. Boschitsch, and Christine L. Solomon, Continuum Dynamics, Inc.

 

Analytical Approach to Helicopter-Ship Certification
Min, Zhou; Chang, Chen; Siang, Seah Choon; Yong, Lek Ngak; Qui, Seah Zuo (Jacqueline); Beng, Wee Teck (Adrian)

 

Analytical Design of a High Performance Stability and Control Augmentation System for a Hingeless Rotor Helicopter
Miyajima, Katsuyuki, NASA

 

Analytical Determination & Experimental Comparison of Performance Degredation on a Helicopter Main Rotor Due to Ice Accretion
R.C. Johnson and A.A. Peterson, Boeing Helicopters and K.D. Korkan and R.K. Britton, Texas A&M University

 

Analytical Determination of Load Distribution in a Statically Indeterminate Face Gear Transmission
H.-W. Chun, R. Filler, J. Tan, The Boeing Company

 

Analytical Development and Experimental Results of a Method for Aerodynamic Contamination Detection
D.J. Cronin and J. M. Vogel, Iowa State University; M.G. Lamb, AERS/Midwest, Inc.

 

Analytical Development and Experimental Results of a Method for Aerodynamic Contamination Detection
D.J. Cronin and J. M. Vogel, Iowa State University; M.G. Lamb, AERS/Midwest, Inc.

 

Analytical Investigation Of Flight Conditions Leading To Unanticipated Right Yaw
Kelly McCool and David Haas, David Taylor Model Basin

 

Analytical Investigation of the Effects of Blade Flexibility, Unsteady Aerodynamics, and Variable Inflow on Helicopter Rotor Stall Characteristics
E. D. Bellinger, UARL

 

Analytical Investigation of UH-60A Flight Blade Airloads and Loads Data
Joon W. Lim, Sterling Software

 

Analytical Methods For LHX Mission And Task Analysis
Bruce E. Hamilton and Howard P. Harper, United Technologies Corporation

 

Analytical Prediction and Flight Test Evaluation of Bell ACAP Helicopter Cabin Noise
Dr. G.P. Mathur, Bell Helicopter Textron and Dr. J.E. Manning and L.R. Quartararo, Cambridge Collaborative, Inc.

 

Analytical Simulation of a Helicopter Mounted Turreted Gun System with Active Control
J. Peters, M. Hashemi-Kia, and M. Toossi, McDonnell Douglas Helicopter Co.

 

Analytical Simulation of ADS-33 Mission Task Elements
Celi, R.

 

Analytical Study of Helicopter Rotor Stall Flutter
F. O. Carta, L. M. Casellini, P. J. Arcidiacono, United Aircraft Research Lab., and H. L. Elman, Sikorsky Aircraft Div.

 

Analytical Techniques for Helicopter Component Reliability
Brown, Michael; Chang, Jung-Hua

 

Analytical Tools for Residual Stress Enhancement of Rotorcraft Damage Tolerance
Stephen Gould, Sikorsky Aircraft Corp; Micheal Urban, Sikorsky Aircraft Corp; James Newman, Mississippi State University; Shak Ismonov, Mississippi State University; Micheal Hill, Hill Engineering

 

Analytical, First Principles Modeling of Elastomeric Dampers
S.Kottapalli, NASA Ames Research Center; O. Bauchau, Georgia Institute of Technology; C. Ju, S. Ozbay, Y. Mehrotra, Materials Technologies Corporation

 

Analyzing Store Separation from Helicopters Using Scale Models
J. Obermark, U.S. Army Aviation and Missile Command; B. Landrum, Univ. of Alabama

 

Analyzing the Engine Entrainment of An Over the Wing Engine Coupled With A Circulation Control Wing
Bryan Blessing, David Marshall, California Polytechnic State University

 

Analyzing the Engine Entrainment of An Over the Wing Engine Coupled With A Circulation Control Wing
Bryan Blessing and David Marshall, Cal Poly

 

Annvestigationnto the Aerodynamics of Trailing Edge Flap and Flap-Tab Airfoils Using CFD and Analytical Methods
Baeder, J.; Jose, Arun; Sitaraman, Jayanarayanan

 

Antennas For The Black Hawk

M.L. Parent, Sikorsky Aircraft Div, UTC

 

Anti-Ice Testing Of The Prewitt Metal Rotor Blade
Robert M. DeWitt

 

Anti-Icing Systems of Helicopter Rotor Blades
Boris S. Sirotinsky and Andrei V. Boulanovsky, M.L. Mil Moscow Helicopter Plant

 

Anti-Icing Systems of Helicopter Rotor Blades
Boris S. Sirotinsky and Andrei V. Boulanovsky, M.L. Mil Moscow Helicopter Plant

 

Antiresonant Rotor Isolation for Vibration Reduction
Desjardins, Rene A., Boeing Vertol Company; Hooper, Euan W., Beoing Vertol Company

 

Antitorque Safety and the RAH-66 Fantail
M.G. Clemmons, Boeing Defense and Space Group, Helicopters Div.

 

Apache Agenda
Derek Paquette, US Army

 

Apache AH Mk1 ODR
Richard Christ and Eric Hitchcock, Boeing Military Aircraft and Roger Redman, AgustaWestland

 

Apache AH Mk1 Operational Data Recording Exercise An Update
Richard Christ and Eric Hitchcock, Boeing Military Aircraft, Roger Redman, AgustaWestland

 

Apache Aviation Turbine Engine Diagnostic System (ATEDS) for the AH-64D Turbine Engine
Merlenbach, Chris

 

Apache Block III Participation in the on the Move Field Exercise
Levin, William; Palich, Mark; Wroblewski, Ken

 

Apache Flight Experience in Operation Iraqi Freedom (OIF) Shows Reduced Incidents of Visual Illusions and Problems with the Monocular Helmet-Mounted Display
Clarence E. Rash, U.S. Army Aeromedical Research Laboratory; Keith L. Hiatt, Headquarters, United States Army Forces Command

 

Apache High-Speed Data Bus
Jeff Davies, The Boeing Company

 

Apache Longbow Aerobatics
Lyndon C. Lamborn, The Boeing Company; Richard A. Lee, The Boeing Company; Mark Metzger, The Boeing Company

 

Apache Longbow Color AMLCD Multipurpose Display Incorporation
J. Kristin Little, The Boeing Company

 

Apache Longbow in Theater Missile Defense Attack Operations
Anthony G. Kraay, The Boeing Company

 

Apache Longbow Integrated Crew Systems: Taking Complexity Out of Radio Communications
Dunlap, K.

 

Apache Mission Processor Software Architecture: Architectural Decisions
Koontz, Ronald

 

Apache Mission Processor Software Architecture: Driving Quality Attributes
Koontz, Ronald

 

Apache Mission Processor Software Architecture: Future Airborne Capability Environment Considerations
Dale Johnson, US Army; Ronald Koontz, The Boeing Company

 

Apache Mission Processor Software: Partitioning & Distributed Display Architecture
Ronald Koontz, The Boeing Company

 

Apache Modernization - The User's Perspective
COL Dave Sale and CPT Gregory J. Lund, U.S. Army TRADOC

 

Apache Prime Vendor Support
Gary S. Nenninger, Boeing

 

Apache Project Office Update
Richard Tyler, US Army

 

Aperiodicity Correction for Rotor Tip Vortex Measurements
Manikandan Ramasamy, UARC/UCSC; Ryan Paetzell, NASA Ames Research Center; Mahendra Bhagwat, US Army AFDD

 

Application Of Probabilistic Methodology In The Development Of Retirement Lives Of Critical Dynamic Components In Rotorcraft
William D. Harris, Boeing Philadelphia; Terry Larchuk, Boeing Philadelphia; Ed Zanoni, Boeing Philadelphia; Lew Zion, Georgia Tech Research Institute

 

Application and Configurationssues of Resin Transfer Molded Composite Transmission Housings: A Program Overview
Cecil, Timothy; Ehinger, R.; Kilmain, C.

 

Application and Validation of High-Order Unstructured Grid Schemes to Vortex-Dominant Flows
Sheng, Chunhua; Zhao, Qiuying

 

Application for the Operational Analysis (OA) of Rotorcraft in Homeland Security, Disaster, and Emergency Response (HSDER) Missions
Barber, John; Gibson, Terry

 

Application of 2GCHAS to the Investigation of Aeromechanical Stability of Hingeless and Bearingless Rotor Helicopters
Robert A. Ormiston, U.S. Army AFDD (ATCOM); Hossein Saberi, Tassos Anastassiades, Advanced Rotorcraft Technology, Inc.

 

Application of a Comprehensive Analytical Model of Rotorcraft Aerodynamics and Dynamics (CAMRAD) to the MDHC AH-64 Helicopter
C.B. Callahan and D.E. Bassett, McDonnell Douglas Helicopter Company

 

Application of a Dependency-Model-Based Health Inference and Troubleshooting Strategy to a HUMS-Enabled Advanced Maintenance Concept
Domagala, Charles; Haste, Deepak; Mathur, Amit

 

Application of a General-Purpose Mechanical Systems Analysis Code to Rotorcraft Dynamics Problems
Andrew S. Elliott, McDonnell Douglas Helicopter Co.; James B. McConville, Mechanical Dynamics, Inc.

 

Application of a High Fidelity Icing Analysis Method of a Model Scale Rotor in Forward Flight
Robert Narducci, The Boeing Company; Stanley Orr, The Boeing Company; Richard Kreeger, NASA Glenn Research Center

 

Application Of A High-Temperature Hybrid Metal/Composite Laminate
J. Donn Hethcock, Rodney H. Jones, B. R. Mullins, Bell Helicopter Textron, Inc.

 

Application of a Local Stress Based Approach in Aluminum Aerospace Joint Design
Michael Urban, Sikorsky Aircraft; Stephen Gould, Sikorsky Aircraft; George Bauer, CAEAI inc; Thomas Meyer, CAEAI inc; Anindya Ghoshal, Army Research Laboratory; Gregory Welsh, United Technologies Research Center; Nathaniel Bordick, AATD

 

Application of a Momentum Source? Model to the RAH-66 Comanche FANTAIL
T. Nygaard, A. Dimanlig, ELORET; T. Meadowcroft, The Boeing Company

 

Application of a Navier-Stokes Free Wake Hybrid Methodology to the Harrington Coaxial Rotor
Jeewoong Kim, Lakshmi N Sankar and JVR Prasad (Georgia Institute of Technology)

 

Application of a New Navier-Stokes Inverse Method to the Design of Advanced Airfoils
J.C. Narramore, Bell Helicopter Textron Inc., J.B. Malone, NASA Langley Research Center and R. Vermeland, CRAY Research, Inc.

 

Application of a Probabilistic Design Environment to the Mission Requirements and Technologies for a Heavy Lift Helicopter
Baker, A.; Mavris, D.; Schrage, D.

 

Application of a Real Time Free Wake Induced Velocity Model in a Naval Rotorcraft Flight Trainer
Jeffrey Keller, Continuum Dynamics, Inc.; Daniel Wachspress, Continuum Dynamics, Inc.; Jacques Hoffler, Naval Air Warfare Center; Nicholas Kachman, Naval Air Warfare Center; James Nichols, Naval Air Warfare Center

 

Application of a Slotted Airfoil for UH-60A Helicopter Performance
Hyeonsoo Yeo, Raytheon ITSS; JoonW. Lim, Army/NASA Rotorcraft Division

 

Application Of A State-Space Wake Model To Tiltrotor Wing Unsteady Aerodynamics
Martin Stettner, Daniel P. Schrage, Georgia Institute of Technology; David A. Peters, Washington University

 

Application Of A Symmetric Total Variation Diminishing Scheme To Aerodynamics And Aeroacoustics Of Rotors
Ebru Usta, Georgia Institute of Technology; Brian E. Wake, United Technologies Research Center; T. Alan Egolf, Sikorsky Aircraft Corporation; Lakshmi N. Sankar, Georgia Institute of Technology

 

Application of a Turbulence Distortion Theory to Predict Helicopter Broadband Noise Due to Inflow Turbulence as a Function of Rotor Thrust
M. Williams and W. Harris, Massachusetts Institute of Technology

 

Application Of A Two-Point Exponential Approximation Method In Optimizing Rotorcraft Airframe Structures
Ashish K. Sareen, Georges M. Fadel, Daniel P. Schrage, Georgia Institute of Technology

 

Application of a Variable-Diameter Rotor System to Advanced VTOL Aircraft
Evan A. Fradenburgh, Sikorsky Aircraft

 

Application of Adaptive Mesh Refinement Technique in Helios to Blade-Vortex Interaction Loading and Rotor Wakes
Joon Lim, US Army AFDD; Andrew Wissink, US Army AFDD; Buvana Jayaraman, Science & Technology Corporation; Arsenio Dimanlig, Science & Technology Corporation

 

Application of Adjoint Optimization Method to Multi-Element Rotorcraft Airfoils
Mark S. Chaffin, Lockheed Martin

 

Application of Advanced Composites for Helicopter Airframe Structure
M. J. Rich, D. W. Lowry, and G. F. Ridgley, Sikorsky Aircraft.

 

Application Of Advanced Manufacturing Technology to the V22 Osprey Composite Airframe Structure
Matthew J. Patterson and Robert L. Pinckney, Boeing Helicopters

 

Application of Advanced Vibration Techniques for Enhancing Bearing Diagnostics on a HUMS-Equipped Fleet
Lance Antolick, RMCI, Inc.; Daniel R. Wade, AED; Nathan G. Brower, RMCI, Inc.

 

Application of Advanced Vibration Techniques for Enhancing Bearing Diagnostics on a HUMS-Equipped Fleet
Lance Antolick, RMCI, Inc.; Daniel R. Wade, AED; Nathan G. Brower, RMCI, Inc.

 

Application of Aeronautical Design Specification 79A to the UH-60L Accessory Gearbox Generator Drive Bearings
Daniel Wade, US Army; Jeremy Branning, RMCI Inc.

 

Application of an Absorber to Reduce Helicopter Vibration Levels
Charles W. Ellis, and Robert Jones, Kaman Aircraft Corp.

 

Application of an Active Joystick in a Rotorcraft UAV Ground Control Station
Stephen Mouritsen, DLR; Roberto Pretolani, Gian Marco Saggiani, and Barbara Teodorani, University of Bologna

 

Application of an Astroquartz Material System to Composite Sandwich Structure
Steven Llorente, Peter Holemans, Boeing Defense & Space Group, Helicopters Div.

 

Application of an Empirical Fatigue Design Method to Predict Fatigue Life During a Development Program
J.P. Norvell

 

Application of an Integrated Decision Support System for Mid-Life Upgrade of Helicopters
Kusumo, R.; Schrage, D.; Sinha, A.

 

Application of Automated Rotor Smoothing Using Continuous Vibration Measurements
Branhof, Robert W.; Grant, Lem; Grabill, Paul; Keller, Jonathan A.

 

Application of Boron/Epoxy to the CH-54B Skycrane R
R. T. Welge, Sikorsky Aircraft

 

Application of CFD Design Technology in Development of the JVX Engine Inlet
G.C. Paynter, J.L. Koncsek, Boeing Military Airplane Co., B. Turczeniuk, Boeing Vertol Co. and D.R. Clark, D.J. Strash, Analytical Methods Inc

 

Application of CFD in the Design of Flow Control Concepts for a Ducted-Fan Configuration
W. Kelly Londenberg, O. John Ohanian, III, AVID LLC

 

Application of CFD/CSD Coupling for Analysis of Rotorcraft Airloads and Blade Loads in Maneuvering Flight
Bhagwat, Mahendra; Ormiston, Robert; Saberi, Hossein; Xin, Hong

 

Application of CFD/CSD to Rotor Aeroelastic Stability in Forward Flight
Ormiston, Robert; Potsdam, Mark; Yeo, Hyeonsoo

 

Application of Classical-Control Techniques for Computer Modeling and Simulation of Helicopter Pilotage Tasks
Robert K. Heffley, Robert Heffley Engineering; Ronald A. Hess, University of California; Yasser Zeyada, University of California

 

Application of Closed-Loop Machining in the Manufacture of Gas Turbines
S.M. Burgess and M.H. Wollowitz, General Electric Co

 

Application of Communication Network Strain Analysis for Existing UAV Network Architecture
A.K. Sinha, R. Kusumo, P.J. Michaelides, Royal Melbourne Institute of Technology

 

Application of Compliant Foil Air Bearings for Oil Free Operation of Advanced Turboshaft Engines
S.D. Spring, M. Kaminske, S. Leone, GE Aviation ? Aircraft Engines; M.V. Drexel, B.H. Ertas, GE Research Center; E.C. Ames, Aviation Applied Technology Directorate; G. Agrawal, D. Burr, M. Brophy, R&D Dynamics

 

Application of Component Mode Synthesis to Modeling the Dynamic Response of Bearingless Main Rotors
R. Sopher and S. Chen, Sikorsky Aircraft Div., UTC

 

Application of Computational Fluid Dynamics During the Conceptual Design of the Bell JHL Quad-Tiltrotor
Lancaster, Glenn; Narramore, Jim; Sheng, Chunhau

 

Application Of Computational Fluid Dynamics To The Design Of The 916 Deepwater UAV
J. C. Narramore, Bell Helicopter Textron, Inc.

 

Application of Computational Fluid Dynamics to the Design of the Bell 429
J.C. Narramore, Bell Helicopter Textron, Inc.

 

Application Of Constraint Suspension Techniques To Diagnosis In Helicopter Caution/Warning Systems
Greg Glenn, McDonne11 Douglas Helicopter Company

 

Application of Damage Tolerance Methodology to Helicopter Dynamic Components Using the Example of a Main Rotor Pitch Link for the AH-1S Helicopter
B.R. Krasnowski and W.W. Spence, Bell Helicopter Textron, and K.M. Rotenberger, U.S. Army Aviation Systems Command

 

Application of Design Optimization Techniques to Rotor Dynamics Problems
M.W. Davis and W.H. Weller, United Technologies Research Center

 

Application Of Design Optimization To Composite Tubes
Aditi Chattopadhyay and Jay Ferreira, Arizona State University

 

Application Of Fatigue Crack Propagation And Strain Survey Testing To The CH-46 Aft Rotor Drive Shaft
Howard S. Faust, Boeing Vertol

 

Application Of Fatigue Crack Propagation And Strain Survey Testing To The CH-46 Aft Rotor Drive Shaft
Howard S. Faust, Boeing Vertol

 

Application Of Finite-Element And Holographic Techniques In The Design Of Turboshaft Engine Components
P.S. Kuo, Avco Lycoming Div.

 

Application of Flexible Fixturing to Aluminum and Composite Bonded Aerospace Structures
Luscher, Anthony; Stephens, Robert

 

Application of Generalized Force Determination to a Full Scale Low Cycle Fatigue Test of the SH-2G Helicopter
C.A. Tomashofski, E.J. Nagy, and P.E. Keary, Kaman Aerospace Corp.`

 

Application of Helicopter Air-to-Air Combat Test (AACT) Data to Current LHX Concerns
F.J. Ebert and N.D. Lappos, Sikorsky Aircraft Division, United Technologies Corp

 

Application of Helicopter Flight Simulators for Training and Research Purposes
P. de Guillenchmidt, Giravions Dorand Company

 

Application Of High Order Schemes To Aerodynamics Of Hovering Rotors
Ebru Usta, Georgia Institute of Technology; Lakshmi N. Sankar, Georgia Institute of Technology

 

Application of Higher Harmonic Control (HHC) to Rotors Operating at High Speed and Maneuvering Flight
K.Q. Nguyen and I. Chopra, University of Maryland

 

Application of Hybrid Methodology to Rotors in Steady and Maneuvering Flight
Bauchau, Olivier; Charles, Bruce; Egolf, Alan; Makinen, Stephen; Rajmohan, Nischint; Sankar, Lakshmi

 

Application of Image Matching Navigation System to Support Approach and Landing of VTOL Vehicle
Zasuwa, Maciej; Narkiewicz, Janusz

 

Application of Ion Fusion Formation to Refurbishment of Aircraft
R. Adams, Honeywell Aerospace - Tempe

 

Application of Low and High Fidelity Simulation Tools to Helicopter Rotor Blade Optimization
Collins, Kyle; Sankar, Lakshmi

 

Application of MADYMO to Helicopter Energy-Absorbing Seat/Occupant System Analysis
Joseph Manning, David Furey, Simula Technologies, Inc.; Bachar Alijundi, TNO-North America; Lindley W. Bark, Simula Technologies, Inc.

 

Application of Manufacturing Science to UH 60 Rotors
Martin, Dave; Medeiros, Paul

 

Application Of Materials Technologies In Small Gas Turbine Engines
C.C. Rhemer, Pratt & Whitney

 

Application of MetalSCAN Oil Debris Monitor to a Fleet of Sea King Helicopters
Dubowski, Doug; Witwer, Dan

 

Application of Model Based Design to Rotorcraft Development
Mike Weaver, BAE Systems

 

Application of Natural Language Processing: Techniques to Marine V-22 Maintenance Data for Populating a CBM-Oriented Database
Huston Bokinsky, Amber McKenzie, Abdel Bayoumi, Rhea McCaslin, Andrew Patterson, University of South Carolina; Manton Matthews, Joseph Schmidley, U.S. Navy; MG. Lester Eisner, SC National Guard

 

Application of Natural Language Processing: Techniques to Marine V-22 Maintenance Data for Populating a CBM-Oriented Database
Huston Bokinsky, Amber McKenzie, Abdel Bayoumi, Rhea McCaslin, Andrew Patterson, University of South Carolina; Manton Matthews, Joseph Schmidley, U.S. Navy; MG. Lester Eisner, SC National Guard

 

Application of Non-Linear Dynamic Inversion to Rotorcraft Flight Control
Howitt, J.

 

Application of Nonlinear Programming Techniques to Dynamic Correlation and Design of Helicopter Structures
T.L.C. Chen, W.J. Twomey, and S. Pizzolato, Sikorsky Aircraft Div., UTC

 

Application of Nonlinear Programming Techniques to Dynamic Correlation and Design of Helicopter Structures
T.L.C. Chen, W.J. Twomey, and S. Pizzolato, Sikorsky Aircraft Div., UTC

 

Application of Optimization Theory to Helicopter Design and Performance Problems
Toshifumi Nekohashi, Tomoari Nagashima, National Defense Academy, Japan

 

Application of Out-of-Plane Warping to Control Rotor Blade Twist
Y. Van Weddingen, O. Bauchau, Georgia Institute of Technology; S. Kottapalli, NASA Ames Research Center; S. Ozbay, Y. Mehrotra, Materials Technologies Corporation

 

Application Of Pilot Induced Oscillations Prediction Criteria To Rotorcraft
Valeria Mariano, Politecnico di Torino; Andrea Ragazzi, AgustaWestland S.p.A; Giorgio Guglieri, Politecnico di Torino

 

Application of Probability Methods to Assess Crash Modeling Uncertainty
Hardy, R.; Lyle, K.; Stockwell, A.

 

Application of Real-Time Flight Simulation for Design of a Helicopter Obstacle Avoidance System
CPT Christopher C. Sullivan, U.S. Army; E. Roberts Wood, U.S. Naval Postgraduate School; Joe DeMaio, U.S. Army AFDD

 

Application of rFlow3D code to performance prediction and the wake structure investigation of wind turbines
Harutaka Oe and Makoto Yamamoto, Tokyo University of Science; Hideaki Sugawara, Ryoyu Systems, Co.; Yasutada Tanabe and Masahiko Sugiura and Takashi Aoyama and Yuichi Matsuo, Japan Aerospace Exploration Agency

 

Application of Rotor Icing Analyses to the Design of a Rotorcraft Deicing System
R.J. Flemming, Sikorsky Aircraft Division, UTC

 

Application Of Safety Oriented System Development Process For Critical Integrated Modular Avionics (IMA)
Mathieu Gester and Serge Germanetti, Eurocopter

 

Application Of Safety Oriented System Development Process For Critical Integrated Modular Avionics (IMA)
Mathieu Gester and Serge Germanetti, Eurocopter

 

Application of Sequential Quadratic Programming to Minimize Smart Active Flap Rotor Hub Loads
Sesi Kottapalli and Jane Leyland, NASA Ames Research Center

 

Application of Sequential Quadratic Programming to Minimize Smart Active Flap Rotor Hub Loads
Sesi Kottapalli and Jane Leyland, NASA Ames Research Center

 

Application of Sequential Quadratic Programming to Rotorcraft Survivability with Power Loss
Matthew Floros, US Army Rresearch Laboratory

 

Application of Shape Memory Alloy Hybrid Composites for Variable-Twist Proprotors
Jung, Sung Nam; Kim, SeongHwan; Park, JaeSang

 

Application Of Skid Landing Gear Dynamic Drop Analysis
Brian E. Stephens, Bell Helicopter Textron, Inc.; William L. Evans, III, Bell Helicopter Textron, Inc.

 

Application of Sound Intensity Technique in Helicopter Acoustics
G.P. Mathur, M.C. Joshi and C.R. Cox, Bell Helicopter Textron, Inc

 

Application Of Statistical Techniques To The Interpretation Of Fatigue Data
Donald L. Henry

 

Application of Task-Pilot-Vehicle (TPV) Models in Flight Simulation
Heffley, Robert

 

Application of the Cepstrum to Remove Echoes from Rotor Acoustic Spectra
R.M. Martin, NASA Langley Research Center and C.L. Burley, PRC Kentron International

 

Application of the Floquet Transition Matrix to Problems of Lifting Rotor Stability
D. A. Peters, McDonnell-Douglas Corp., and Prof. K. H. Hohenemser, Washington University

 

Application of the Helicopter in Connection with Surface Transport
James, Russell B.

 

Application of the IMD HUMS to the UH-60A Blackhawk
Dora, Ray; Baker, Treven; Hess, Robert

 

Application of the Joint Technical Architecture (JTA) to the Navy MultiMission Helicopter (MMH) Program
Thomas D. Gaska, Lockheed Martin Federal Systems

 

Application of the Wide-Field Shadowgraph Technique to Helicopters in Forward Flight
Jeffrey S. Light, NASA Ames Research Center; Alexandra A. Frerking, Sterling Federal Systems; Thomas R. Norman, NASA Ames Research Center

 

Application Of Three-Component PIV To A Hovering Rotor Wake
James T. Heineck, NASA Ames Research Center; Gloria K. Yamauchi, NASA Ames Research Center; Alan J. Wadcock, Aerospace Computing, Inc.; Luiz Lourenco, Florida State/Florida A&M University; Anita I. Abrego, NASA Ames Research Center

 

Application of Uncooled Ceramic Matrix Composite Power Turbine Blades for Performance Improvement of Advanced Turboshaft Engines
Hogan, Mike; Kinney, Steve; Lewis, Douglas; McMahon, John

 

Application of Uncooled Ceramic Matrix Composite Power Turbine Blades for Performance Improvement of Advanced Turboshaft Engines
S.D. Spring, M.T. Hogan, D.A. Lewis, J.D. Steibel, GE Aviation ? Aircraft Engines; S. Kinney, Aviation Applied Technology Directorate

 

Application of Vortex Visualization Test Techniques to Rotor Noise Research
R. H. Spencer, Boeing/Vertol

 

Applications of Antiresonance Theory to Helicopters
Felton D. Bartlett, Jr., and William G. Flannelly, Kaman Aerospace Corp. (Standby)

 

Applications Of Generalized Dynamic Wake Theory To The Flow In A Rotor Wake
Zhongyang Fei and David Peters, Washington University in St louis

 

Applications of Infrared Technology to Helicopter Flight Testing
David, Ramel; Laurent, Girard; Philippe, Herv?

 

Applications of Intelligent Autonomy Technologies to Improved UAV Reliability and Sense and Avoid Operations in Uncontrolled Airspace
Robert M. Williams, Aerospace Consultant

 

Applications of Operational Analysis to the Preliminary Design Process
M. Dinneen, Sikorsky Aircraft Division, UTC and P. Donnelly, Boeing Vertol Co

 

Applications of Space Shuttle Technology to Next Generation Flight Control Architectures
Donald L. McCorvey III, Fernando Dones, Boeing, NASA

 

Applications Of Stress Models To Rotor Blade Design Analysis
Thomas H. Purcell

 

Applications of the Induced Power Model and Performance of Conventional and Advanced Rotorcraft
R. Ormiston, Aeroflightdynamics Directorate, U.S. Army RDECOM

 

Applications of Virtual Monitoring of Loads to Engineering Decision Making
Raymond J. Beale Jr., Sikorsky Aircraft

 

Applied Aerodynamics of Circulation Control Airfoils and Rotors
E.O. Rogers, A.W. Schwartz and J.S. Abramson, David W. Taylor Naval Ship Research and Development Center

 

Applying A Health & Usage Monitoring System (HUMS) in the Civil Environment
Dave Squires, Cougar Helicopters Inc.

 

Applying A Health & Usage Monitoring System (HUMS) in the Civil Environment
Dave Squires, Cougar Helicopters Inc.

 

Applying Fem for Development of an Impact Resistant Aircraft Windshield
Zi Lu, Jeremy Schadler and Cheng-Ho Tho, Bell Helicopter Textron

 

Applying High-Speed Machining Techniques On Rotor Grip Configurations
Edmund P. Leigh, Bell Helicopter Textron, Inc.; Jiri Tlusty, University of Florida; John Schueller, University of Florida

 

Applying PHM to the Shaft Driven LiftFan
O.A. (Bud) Watts, Allison Advanced Development Company

 

Applying Rotorcraft Technology in the New Millennium: U.S. Army R&D Flight Test Update
LTC Jeffrey A. Trang, USA, U.S. Army Aviation and Missile Command; LTC Allen L. Peterson, USA, PEO Aviation; CW4 John Wood, USA, U.S. Army Aviation and Missile Command

 

Applying Software Safety Methodologies to the SH-2G(A) Glass Cockpit
Hoagland, Michael V.

 

Applying Technology for Cost Effective Upgrades
Tim Bartley, Westland Helicopters, Ltd.

 

Applying Virtual Simulation in Operational Testing of Apache Block III Levels of Interoperability with Unmanned Aerial Systems
Scott Swinsick, Boeing Technical Fellow, and Christa Luna, The Boeing Company

 

Appraisal of Digital Terrain Elevation Data for Low-Altitude Flight
R.E. Zelenka and H.N. Swenson, NASA Ames Research Center

 

Approach Vibration Control of the RSRA/X-wing Vehicle Using A Time Domain Approach
R.W. DuVal and H.A. Saberi, Advanced Rotorcraft Technology, Inc.

 

Approaches for Improving Rotor Load Identification Technology
Shoushen Liu, Georgia Institute of Technology; Daniel P. Schrage, Georgia Institute of Technology; Jerry P. Higman, U.S. Army

 

Approximate Actuator Disk Model Of A Rotor
Aviv Rosen, Technion - Israel Institute of Technology

 

April 2007
Journal of the American Helicopter Society, Volume 52 - Number 2

  • Design Optimization for Improved Tiltrotor Whirl Flutter Stability - Hathaway, Eric; Gandhi, F.
  • Toward Noise Abatement Flight Procedure Design: DLR Rotorcraft Noise Ground Footprints Model - Yu, Jianping; Buchholz, H.
  • Experimental Investigations of Rotor-Fuselage Aerodynamic Interactions - Le Pape, A.; Gatard, J.; Monnier, J.-C.
  • High Resolution Wake Capturing Methodology for Hovering Rotors - Duraisamy, Karthikeyan; Baeder, J.
  • Evaluation of a Rotorcraft Autorotation Training Display on a Commercial Flight Training Device - Aponso, Bimal L.; Lee, D.; Bachelder, E.N.
  • How Long Do Pilots Look Forward? Prospective Visual Guidance in Terrain-Hugging Flight - Padfield, Gareth D.; Clark, G.; Taghizad, A.
  • Miniature Trailing-Edge Effectors for Rotorcraft Performance Enhancement - Kinzel, Michael P.; Maughmer, M.D.; Lesieutre, G.A.
  • Multi-Terrain Impact Tests and Simulations of an Energy Absorbing Fuselage Section - Fasanella, Edwin L.; Jackson, K.E.; Lyle, K.H.; Sparks, C.E.;Sareen, A.K.

 

April 2008
Journal of the American Helicopter Society, Volume 53 - Number 2

  • Robust-Adaptive Magnetic Bearing Control of Flexible Matrix Composite Rotorcraft Driveline - DeSmidt, Hans A.; Wang, K.W.; Smith, E.C.
  • Main Rotor-Tail Rotor Interaction and Its Implications for Helicopter Directional Control - Fletcher, Timothy M.; Brown, R.E.
  • Prediction of Vortex Ring State Boundary of a Helicopter in Descending Flight by Simulation - Basset, Pierre-Marie; Chen, C.; Prasad, J.V.R.; Kolb, S.
  • Assessment of Active Controls for Rotor Performance Enhancements - Yeo, Hyeonsoo
  • Prediction of Air and Ground Resonance Stability of Soft-Implane Tiltrotors Using a Semispan Analytical Model - Howard, Anna K.T.; Smith, E.C.
  • Soft-Inplane Tiltrotor Aeromechanics Investigation Using Two Comprehensive Multibody Solvers - Masarati, Pierangelo; Piatak, D.J.; Quaranta, G.; Singleton, J.D.; Shen, J.
  • Prediction of Rotor Structural Loads with Comprehensive Analysis - Yeo, Hyeonsoo; Johnson, W.

 

April 2009
Journal of the American Helicopter Society, Volume 54 - Number 2

  • Coupled Thrust and Vorticity Dynamics during Vortex Ring State - Omer Savas; Green, R.B.; Caradonna, F.X.
  • Performance Analysis of the Slowed-Rotor Compound Helicopter Configuration - Matthew W. Floros; Johnson, W.
  • Experiments and Analysis on Postbuckling Behavior of Stringer-Stiffened Laminated Composite Helicopter Tailplane - Chiara Bisagni; Giavotto, V.
  • Leveraging Information to Support Military Flight Operations Quality Assurance - Miguel A. Morales; Haas, D.J.; Fuller, B.L.; Chavez, T.
  • Time-Accurate Ship Airwake and Unsteady Aerodynamic Loads Modeling for Maritime Helicopter Simulation - Steven D. Hodge; Zan, S.; Roper, D.M.; Padfield, G.D.; Owen, I.
  • Procedures for Measuring the Turbulence Characteristics of Rotor Blade Tip Vortices - Manikandan Ramasamy; Johnson, B.; Huismann, T.; Leishman, J. G.
  • Technical Note: Improved Computational Strategies for Rotor Blades Presenting High Gradients in Sectional Properties - Olivier A. Bauchau; Epple, A.

 

April 2011
Journal of the American Helicopter Society, Volume 56 - Number 2

  • The Nature of Vortex Ring State - Albert Brand; Mark Dreier; Ron Kisor; Tom Wood
  • Effect of Blade Number on Induced Power in Hover - Mahendra J. Bhagwat
  • Three-Dimensional Finite Element Formulation and Scalable Domain Decomposition for High-Fidelity Rotor Dynamic Analysis - Anubhav Datta; Wayne Johnson
  •  A Framework for Robust Rotorcraft Flight Control Design - Ronald A. Hess
  • Experimental Optimization of MAV-Scale Cycloidal Rotor Performance - Moble Benedict; Tejaswi Jarugumilli; Inderjit Chopra
  • A Review of Rotor Wake Physics and Modeling - Narayanan M. Komerath; Marilyn J. Smith; Chee Tung
  • Local Terrain Mapping for Obstacle Avoidance Using Monocular Vision - Marlow, Sean Quinn; Langelaan, Jack W.
  • System Identification of a Rotary-Wing Micro Air Vehicle - Conroy, Joseph K.; Humbert, J. Sean; Pines, Darryll J.

 

April 2012
Journal of the American Helicopter Society

Use of Rotor State Feedback to Improve Closed-Loop Stability and Handling Qualities - Horn, Joseph F.; Guo, Wei; Ozdemir, Gurbuz Taha

A Surrogate-Based Approach to Reduced-Order Dynamic Stall Modeling Experimental Studies to Understand the Hover and Forward Flight Performance of a MAV-Scale Flapping Wing Concept - Glaz, Bryan; Liu, Li; Friedmann, Peretz P.; Bain, Jeremy; Sankar, Lakshmi N.

Extracting Stochastic Airwake Models from a Database for Engineering Analysis and Simulation - Malhan, Ria; Benedict, Moble; Chopra, Inderjit

Load Reduction in Lead-Lag Dampers by Speed-Scheduled Aperture and Modulated Control of a Bypass Valve - Gaonkar, Gopal H.; Mohan, Ranjith

Icing Environment Rotor Test Stand Liquid Water Content Measurement Procedures and Ice Shape Correlation - Bottasso, Carlo L.; Cacciola, Stefano; Croce, Alessandro; Dozio, Lorenzo

Assessment of Scavenge Efficiency for a Helicopter Particle Separation System - Jiang, L.Y.; Han, Yiqiang; Brouwers, Edward W.; Smith, Edward C.

Rotor Vibration Reduction Using an Embedded Spanwise Absorber - Austruy, Julien; Benner, M.; Bird, J.

 

April 2013
Journal of the American Helicopter Society
Volume 57 - Number 4

 

Architectural Impact of Blending Machine Intelligence Technology with Full Spectrum Rotorcraft Operations
F.E. Huber, IBM Federal Systems Division and K. Wroblewski, McDonnell Douglas Helicopter Co.

 

Architecture for a Light Helicopter HUMS
Eric Bechhoefer, NRG Systems; Mike Augustin, IVHM Inc and Michael Kingsley, Sikorsky Aircraft Company

 

Architecture for Dynamic Component Life Tracking in Advanced HUMS, RFID, and Direct Load Sensor Environment
Algera, Douglas; Bradfield, Scott; Flores, Enrique; Iyyer, Nagaraja; McColl, Chance; Phan, Nam; Sarkar, Subhasis

 

Architecture Framework for Aviation Systems Participating in Network Centric Operations Developmental Flight Tests
Mark E. Palich, Dale L. Johnson, and Michael W. Donnerstein, The Boeing Company

 

Arctic Operations
Christian Drouin, Royal Canadian Air Force

 

Are Two Always Better Than One?
S.A. Hanvey and C.A. Parlier, Hughes Helicopters, Inc.

 

ARH-70A Armed Reconnaissance Mission
Neil Thurgood, US Army

 

Arm Gesture Control of Mini-Rotorcraft Swarms
Finton, David; Murray, Paul; Troy, James; Wojcik, Richard

 

Armed Helicopters - A Forecast
Lt. Col. John W. Oswalt, USA

 

Armed Scout Helicopter
Mike Herbst, US Army

 

Armed Scout Helicopter
Mike Herbst, US Army

 

Armed Scout Helicopter Update
Robert Grigsby, US Army

 

Army / Navy Operational Evaluation of Offshore Discharge of Containerships
LtC. L. J. McConnell, USA

 

Army Air Rescue Operations
Captain Lyons, James

 

Army Apache Modernization
US Army

 

Army Armed Scout Helos
Keith Robinson, US Army

 

Army Aviation
Quackenbush, U.S. Army

 

Army Aviation
Robert B. Quackenbush, US Army

 

Army Aviation Fusion of Sensor-Pushed and Agent-Pulled Information
Angela M. Pawlowski, Lockheed Martin Advanced Technology Laboratories; Craig W. Stoneking, Lockheed Martin Advanced Technology Laboratories

 

Army Aviation Logistics Infrastructure for the Twenty First Century
Martin F. Walsh, Jr., US Army

 

Army Aviation Maintenance Data and Supportability Interface
T.A. Geoffroy and T.V. Stokes, U.S. Army Aviation Systems Command

 

Army Aviation Modernization
LTC Freddie Mills, U.S. Army

 

Army Aviation Operations [Presentation]
Brigadier Mick Prictor

 

Army Aviation PEO/PM Agenda
Tim Crosby, US Army

 

Army Aviation Propulsion S&T Overview
Gary Butler, US Army

 

Army Aviation Science and Technology Program
Dr. James C. Bradas, AMRDEC

 

Army Aviation Situational Awareness Through Intelligent Agent-Based Discovery, Propagation, and Fusion of Information
Jameson, Stephen; Stoneking, Craig

 

Army DT Airworthiness Release Process
Dr. Robert King, Aviation Engineering Directorate

 

Army Helicopter Crashworthiness: Loading the Battlefield Dice in Our Favor
K.F. Smith, Applied Technology Laboratory, AVSCOM

 

Army Helicopter Performance Trends
R. B. Lewis II, USAASTA

 

Army Preliminary Evaluation of the HLH ATC Demonstrator Fly-by-Wire Flight Control System AFCS
D. R. Simon, J. L. Terry, Jr., and J. C. Savage, USAAMRDL, Eustis Directorate

 

Army Rotorcraft Flight Safety Parts Alternate Source Qualification
L.R. Heitzmann and P.F. Maloney, Dayton T. Brown, Inc.; and R.W. Arden, U.S. Army AATD

 

Army S&T Engine Demonstrator Efforts: Advanced Affordable Turbine Engine (AATE) and Future Affordable Turbine Engine (FATE)
Anastasia Kozup, Aviation Applied Technology Directorate

 

Army Utility Helos
L. Neil Thurgood, B. Keith Roberson, US Army

 

Army Vertical Take Off and Landing (VTOL) Update
Matthew G. Munster, US Army

 

Army Vibration Survey Methods and Results
Emmett J. Laing, USA, ASTA

 

Army Aviation Service Life Analysis  (Phase II) Executive Brief
Beck, US Army

 

Articulated Blade-Element Rotor Model with Variable Radius and RPM, Flap-Lag-Pitch Hinge Arrangement, Rigid Blades and Torque Offset
Ivan Grill, Boeing Rotorcraft Division

 

Articulated Blade-Element Rotor Model with Variable Radius and RPM, Flap-Lag-Pitch Hinge Arrangement, Rigid Blades and Torque Offset
Ivan Grill, The Boeing Company

 

Artificial Force Feel In The BA609 Tiltrotor
Anil Mehra, Bell Helicopter Textron, Inc.

 

ASD(R&E) Perspective
Joseph Doychak, Christopher A. Martin, DoD

 

Asian - Soviet Joint Helicopters Operations
T.P. Lloyd

 

Asian Vertiflite Seminar 13 February 1990 The Future - Tiltrotor Aircraft
Philip C. Norwine; Warren A. Samouce

 

Asian/Australian Rotorcraft Forum (Tianjin, China, Sept. 8-11, 2013)
various

 

Aspects of Flight Testing HUMS Technology
Robert Hess, James Barnes, Bryan St. George, Goodrich Fuel and Utility Systems

 

Assesment of Helicopter Hub Drag Prediction with an Unstructured Flow Solver
B. Wake; E. Hagen; S. Ochs; C. Matalanis; M. Scott; T. Egolf;

 

Assessing Bearing Health for Helicopter Power Train Systems
Chin, Harrison H.; Mayhew, Eric; Green, David L.

 

Assessing Crew Information Requirements For Advanced Diagnostic And Prognostic Systems: Implications For Interface And Training Design
Randall L. Oser, Rene'e J. Stout, and Robert Tyler, Naval Air Warfare Center

 

Assessing Crew Information Requirements For Advanced Diagnostic And Prognostic Systems: Implications For Interface And Training Design
Randall L. Oser, Rene'e J. Stout, and Robert Tyler, Naval Air Warfare Center

 

Assessing Rotorcraft Airframe Durability and Damage Tolerance
Avinash Sarlashkar, Darryl Toni, Ted Meyer, Matt Harrigan, Sikorsky Aircraft Corporation (SAC); Nathaniel Bordick, U.S. Army

 

Assessing Sustained Fatigue Damage in Traditionally-Benign Steady-State Helicopter Flight Conditions
Robert Benton, Jeremiah Hardman and Jung-Hua Chang, US Army Aviation Engineering Directorate

 

Assessing the Fidelity of a Human-in-the-Loop Helicopter Flight Research Simulator
Sylvain Manso and Kate Bourne, DSTO

 

Assessing the Impact of Mission Requirements, Vehicle Attributes, Technologies and Uncertainty in Rotorcraft System Design
Baker, Andrew P.; Mavris, Dimitri N.; Schrage, D. P.

 

Assessing the Impact of Reduced Airspeed on Tiltrotor Support to Ground Combat
A.S. Warshawsky, D.U. Olness, and M.J. Uzelac, Lawrence Livermore National Laboratory

 

Assessment and Calibration of Semi-Empirical Models for Predicting Pollutant Emissions of the Erica Tiltrotor Turboshaft Engine
Lorenzo Dal Mas and Ernesto Benini, University of Padua; Rita Ponza, HIT09 srl

 

Assessment of a Crashworthy Fuel Tank Finite Element Model for Ground Impact Analysis
Anghileri, Marco; Castelletti, Luigi; Francesconi, Edoardo; Invernizzi, Fabio; Tirelli, Maurizio

 

Assessment of Active Controls for Rotor Performance Enhancement
H. Yeo, U.S Army, AFDD

 

Assessment of Aerodynamic Challenges of a Variable-Speed Power Turbine for Large Civil Tilt-Rotor Application
Welch, Gerard

 

Assessment of Beam Modeling Methods for Rotor Blade Applications
Vitali V. Volovoi, Georgia Institute of Technology; Dewey H. Hodges, Georgia Institute of Technology; Carlos E. S. Cesnik, Massachusetts Institute of Technology; Bogdan Popescu, Bell Helicopter Textron

 

Assessment of BVI Noise Reduction by an Active Tab through Numerical Simulations
Hideaki Sugawara Research Engineer, Ryoyu Systems Co., Ltd.

 

Assessment Of Cargo Space Seating Performance Applicable To Pave Hawk And Black Hawk Aircraft During Helicopter Mishaps
Nathan Wright, Air Force Research Laboratory

 

Assessment of CFD/CSD Analytical Tools for Improved Rotor Loads

Loren Ahaus, Bell Helicopter Textron Inc.; Stephen Makinen, Sikorsky Aircraft Corporation; Ted Meadowcroft and Hormoz Tadghighi, The Boeing Company; Lakshmi Sankar, Georgia Institute of Technology; James Baeder, University of Maryland

 

Assessment of CFD/CSD Analytical Tools for Improved Rotor Loads

Loren Ahaus, Bell Helicopter Textron Inc.; Stephen Makinen, Sikorsky Aircraft Corporation; Ted Meadowcroft and Hormoz Tadghighi, The Boeing Company; Lakshmi Sankar, Georgia Institute of Technology; James Baeder, University of Maryland

 

Assessment of CFD/CSD Coupled Aeroelastic Analysis Solution for HART II Rotor Incorporating Fuselage Effects
Jung-Hwan Sa, Konkuk University; Young-Hyun You, Konkuk University; Jae-Sang Park, Konkuk University; Sung Jung, Konkuk University; Soo-Hyung Park, Konkuk University; Yung Yu, Konkuk University

 

Assessment of Comprehensive Analysis Calculation of Airloads on Helicopter Rotors
H. Yeo, Raytheon ITSS; W. Johnson, NASA Ames

 

Assessment of Comprehensive Analysis Calculation of Structural Loads on Rotors
Yeo, Hyeonsoo; Johnson, Wayne

 

Assessment Of Handling Qualities For The Shipborne Recovery Task - ADS 33 (Maritime)
Stephan J.R.P. Carignan, Flight Research Laboratory; Arthur W. Gubbels, Flight Research Laboratory; Kris Ellis, Flight Research Laboratory

 

Assessment of Helicopter Wire Strike Accidents and Safety Warning and Protection Devices
Nagaraj, Vengalattore T.; Chopra, Inderjit

 

Assessment of Ice Accretion Effects on Rotor Dynamics via Multi-Body and CFD Approaches
Daniel Kelly and Habibollah Fouladi and Wagdi Habashi and Marco Fossati, McGill University; Roberto Alicino and Giuseppe Quaranta and Pierangelo Masarati, Politecnico di Milano

 

Assessment of Maintenance Need for Condition-Based Maintenance Development
Georg Wurzel, Eurocopter Deutschland GmbH; Andreas Doleschel, Eurocopter Deutschland GmbH; Michael Weigand, Vienna University of Technology; Falk Hoffmann, Eurocopter Deutschland GmbH

 

Assessment of Maintenance Need for Condition-Based Maintenance Development
Georg Wurzel, Eurocopter Deutschland GmbH; Andreas Doleschel, Eurocopter Deutschland GmbH; Michael Weigand, Vienna University of Technology; Falk Hoffmann, Eurocopter Deutschland GmbH

 

Assessment of Maintenance Need for Condition-Based Maintenance Development
Georg Wurzel, Eurocopter Deutschland GmbH; Andreas Doleschel, Eurocopter Deutschland GmbH; Michael Weigand, Vienna University of Technology; Falk Hoffmann, Eurocopter Deutschland GmbH

 

Assessment of Morphing Wings on the horizontal stabilizer of a Tiltrotor
Ernesto Benini, University of Padova, Nicola Simioni and Rita Ponza, HIT09 S.r.l.

 

Assessment of Predictive Capability of Aeromechanics Methods
William G. Bousman, Quercus Associates SL; Thomas Norman, NASA Ames

 

Assessment of Rotorcraft Agility and Maneuverability with a Pilot-in-the-Loop Simulation
L.S. Levine, F.W. Warburton, Sikorsky Aircraft Division, United Technologies Corp. and H.C. Curtiss Jr., Princeton University

 

Assessment of Rotorcraft Agility and Maneuverability with a Pilot-in-the-Loop Simulation
L.S. Levine, F.W. Warburton, Sikorsky Aircraft Division, United Technologies Corp. and H.C. Curtiss Jr., Princeton University

 

Assessment of Shell and Beam Elements for Modeling Rotorcraft Blades
Hao Kang, Chongseok Chang and Hossein Saberi, Advanced Rotorcraft Technology, Inc. and Robert Ormiston, US Army AFDD (AMRDEC)

 

Assessment of Simulation Fidelity Using Measurements of Piloting Technique in Flight
S.W. Ferguson, W.F. Clement, Systems Technology Inc., W.B.Cleveland, NASA Ames Research Center, and D.L. Key, U.S. Army Aeromechanics Laboratory (AVRADCOM)

 

Assessment of Structural Damage in Composites Utilizing Acoustic Emission Technology
W.C. Boyce, Sikorsky Aircraft and R.K. Miller, United Technologies Researche Center, Divisions of United Technologies Corp

 

Assessment of the Engine Installation Performance of a Redesigned Tiltrotor Intake System
Gianluigi Mist?, Tommaso Nibale and Andrea Garavello and Ernesto Benini, University of Padova

 

Assessment Of Tip Driven And Shaft Driven Rotors For Heavy Lift Applications
Vengalattore T. Nagaraj, Inderjit Chopra, University of Maryland

 

Assessment Of Vertical Axis Handling Qualities For The Shipborne Recovery Task - ADS 33 (Maritime)
Stephan J.R.P. Carignan, National Research Council of Canada; Arthur W. Gubbels, National Research Council of Canada

 

Assessment of VRS Risk During Steep Approaches
L. Binet, A. Taghizad, ONERA

 

Assuring Human-Centeredness in Intelligent Rotorcraft Cockpits: Using Crew Intent Estimation to Coordinate RPA Functions
Robert C. Andes, Jr., Applied Systems Intelligence, Inc.

 

Assuring Human-Centeredness in Intelligent Rotorcraft Cockpits: Using Crew Intent Estimation to Coordinate RPA Functions
Robert C. Andes, Jr., Applied Systems Intelligence, Inc.

 

ASTEC: Affordable Power Today
Kate Calvert, Rolls-Royce

 

Asymmetric Acoustic Scattering for Structural Health Monitoring
Bordick, Nathaniel; Costiner, Sorin; Davis, Mark; Ghoshal, Anindya; Manes, Enrico; Urban, Michael; Welsh, Gregory; Winston, Howard

 

At-Sea Verification of Simulated Dynamic Interface Test Techniques
Dr. Bernard Ferrier, Hoffman Engineering Corp.; Dr. John Duncan, MOD DE&S; Dean Carico, NAVAIR

 

Atlas Human Powered Helicopter
Cameron Robertson, University of Toronto

 

Attack Helicopter Missions - Past, Present And Future
COL Cecil L, Shrader, TRADOC

 

Attack Helicopter Missions - Past, Present And Future
COL Cecil L, Shrader, TRADOC

 

Attacking the Maintenace Problem through Mechanical Design
Doman, Glidden S., Doman-Frasier Helicopters, Inc.

 

Attaining Fatigue and Damage Tolerance Life Goals in Helicopter Bushed Assemblies
Len Reid, Fatigue Technology Inc.

 

ATTHeS - A Helicopter In-Flight Simulator with High Bandwidth Capability
G. Bouwer, H. Pausder, and W. von Guernhagen, DLR

 

Audiotactile Displays for Improving Situation Awareness and Mitigating Spatial Disorientation
Christopher Brill, Old Dominion University; Ben Lawson and Angus Rupert, U.S. Army Aeromedical Research Laboratory; and Isabella Gagliano, Old Dominion University

 

Augmented Systems for a Personal Aerial Vehicle Using a Civil Light Helicopter Model
Stefano Geluardi, University of Pisa; Frank M. Nieuwenhuizen, Max Planck Institute for Biological Cybernetics; Lorenzo Pollini, University of Pisa;  and Heinrich H. Bülthoff, Korea University

 

Augmenting the Vigilante? Unmanned Aerial Vehicle System for Safe, Effective, and Flexible Employment of 2.75-Inch Rockets
Johnson, Kenneth B.

 

Augustine’s Law and Unit Cost Growth in the Rotorcraft Industry
Eric Streich, The Boeing Company

 

Aurora VTOL Technologies
Jim Paduano, Michael Piedmonte, and John Wissler, Aurora Flight Sciences

 

Auto-Coded Digital Flight Control Laws Using ARINC-653 Partitioning
Rudley, Frank M.

 

Autogiro Company of America vs. the United States No. 50328, 181 Ct. Cl., 384 F.2. 391 (1967) - How the Longest Patent Case in U.S. History Defined the Rotary-Wing Legacy of Harold F. Pitcairn
Bisanz, Matthew

 

Autogiro Handling Qualities Assessment
Bagiev, Marat; Houston, Stewart S.; Thomson, Douglas G.

 

Automated Autorotation For Unmanned Rotorcraft Recovery
Bimal L. Aponso, Edward N. Bachelder, Ph.D., and Dongchan Lee, Ph.D., Systems Technology, Inc.

 

Automated C3I For Target Data Dissemination
Barry Driggs, IBM Federal Systems

 

Automated Combustor Hole Drilling and Inspection System
F.R. Moskal III, Garrett Engine Division, Allied Signal Aerospace

 

Automated Composite Ply Verification
Al Trudeau, Sikorsky Aircraft Corp.; Jeffry Purse, Sikorsky Aircraft Corp.; Scott Blake, Assembly Guidance Systems, Inc.

 

Automated Composite Tape Laying
D.W. Murrell, Bell Helicopter Textron, Inc

 

Automated Coordinate Measuring Machine to Inspect Twist and Contour of Main Rotor Blades at Bell Helicopter Textron
M.G. Huffman, Bell Helicopter Textron

 

Automated Damage Assessment for Improved Readiness of Fielded Aircraft
Harris, Aaron; McCarthy, Dennis; Wilke, Dan

 

Automated Data Translation for Avionics Health Management through Intelligent Evidence Streams and Databases
Byington, Carl; Donovan, Bryan P.; Kalgren, Patrick

 

Automated Design of Noise-Minimal, Safe Rotorcraft Trajectories
Robert Morris, NASA Ames Research Center; K. Brent Venable, University of Padova, Italy and James Lindsey, Monterey Technologies

 

Automated Design of Quiet Trajectories Using Land Use Models
Kristen Venable, Tulane University; Matthew Johnson, Institute for Human and Machine Cognition; Robert Morris, NASA Ames Research Center

 

Automated Design of Quiet Trajectories Using Land Use Models
Robert Morris, NASA Ames Research Center; Matthew Johnson, Institute for Human and Machine Cognition; Kristen Venable, Tulane University

 

Automated Eddy Current Inspections For Turbine Engine Component Life Extensions
John Caraway, U S Army; Craig Benson, Veridian, Inc.

 

Automated Generation of Airfoil Performance Tables using a Two-Dimensional Navier-Stokes Solver
E. Mayda, C. van Dam, UC Davis

 

Automated Harness Design and Process Planning
George P. Geanuracos and Jeanette Hollis, Sikorsky Aircraft Div, UTC

 

Automated Helicopter Survivability Planning
John O'Neill, Lockheed Martin Systems Integration; Torrey Deas, US Army

 

Automated Helicopter Survivability Planning
John O’Neill, Lockheed Martin; Torrey Deas, US Army

 

Automated Helicopter Vibration Diagnostics for the US Army and National Guard
Paul Grabill, Intelligent Automation Corporation; Dr. John Berry, US Army AMCOM-AMRDEC; CW5 Lem Grant, South Carolina Army National Guard; Jesse Porter, US Army AMCOM-RTTC

 

Automated Inspection and Precision Grinding of Spiral Bevel Gears
A.J. Lemanski and H. Frint, Sikorsky Aircraft Division, United Technologies Corporation

 

Automated Layup of Composite Structures
E. Frank

 

Automated Power Assessment for Helicopter Turboshaft Engines
Litt, Jonathan; Simon, Donald

 

Automated Power Assurance Refinement for a Turboshaft Engine
Alvaro Soares, GE Aviation; Brian LeFevre and Mark Davis, Sikorsky Aircraft Corporation; Treven Baker, U.S. Army Aviation Development Directorate

 

Automated Rotor Blade Robotic Surface Finishing
Panayiotis S. Shiakolas, University of Texas; Tommy J. Lawley, University of Texas

 

Automated Tuning of Airframe Vibration by Structural Optimization
H. Miura and M. Chargin, NASA Ames Research Center

 

Automated Vibration Management Program for the UH60 Blackhawk
P. Grabill, Scientific Atlanta and L. Grant, South Carolina Army National Guard

 

Automated, Integrated UAV Health Monitoring System: Flight Test Case Study
Timothy E. Lee, Mary Jayne Cribbs, and John C. Krainski, The Boeing Company

 

Automatic Control of Helicopters
Delvin E. Kendall, Jr.

 

Automatic Flight Control System (AFCS) Honeywell SPZ-7600 for Search and Rescue Helicopters
B. Eddy, Honeywell, Inc.

 

Automatic Flight Control System for the Anglo-Italian EH101 Helicopter
J. Meadows and G.R. Parr, Smiths Industries

 

Automatic Landing Detection of Helicopters Equipped with Landing Skid
Steffen Greiser, DLR; Robin Lantzsch, DLR; Andreas Buschbaum, 38108 Valter B?hm, TU Ilmenau

 

Automatic Limit Detection and Avoidance for Heli-UAVs
Ilkay Yavrucuk and J.V.R. Prasad, Georgia Institute of Technology

 

Automatic Limit Detection and Avoidance for Unmanned Helicopters
Ilkay Yavrucuk, Georgia Institute of Technology; J.V.R. Prasad, Georgia Institute of Technology

 

Automatic Link Establishment - The Key to Reliable Helicopter NOE Communications
G.A. Bradley, Bendix / King

 

Automatic Scanning Inspection Of Composite Helicopter Structures Using An Advanced Technology Fluoroscope System

R.H. Porter & B.J. Hunter, Bell Helicopter Textron

 

Automatic Stabilization Equipment For The Army/Hughes YAH-64 Advanced Attack Helicopter
J.E. Engle, Sperry Flight Systems

 

Automatic STOVL Recovery
Gordon Ingle, Luke Gillett, QinetiQ

 

Automating Rotorcraft Parts Life Tracking using RF rechargeable semi-passive RFID
Mike Augustin and Charles Sanzone and Bud Coleman, Benz Airborne Systems; Nam Phan and Daniel Liebschultz, Navy

 

Autonomic Logistics: The Science Behind the Slogan
Dr. William Scheuren, DARPA; Leo Fila, Geoff Goodman, Sue Morris, Reginald Parker, Centra Technology

 

Autonomous Air System Technologies Development at the Army Research Laboratory
Mark W. Nixon, Vehicles Technology Directorate

 

Autonomous Autorotation Flights of Helicopter UAVs to Known Landing Sites
Alles, Wolfgang; Holsten, Johanna; Loechelt, Sven

 

Autonomous Control and Path Planning for Autorotation of Unmanned Helicopters
Thanan Yomchinda, Joseph Horn and Jacob Langelaan, The Pennsylvania State University

 

Autonomous Emergency Landing of a Helicopter: Motion Planning with Hard Time-Constraints
Sanjiban Choudhury and Sebastian Scherer and Sanjiv Singh, Carnegie Mellon University

 

Autonomous Exploration and Navigation Strategies for MAVs
Sai Vemprala and Srikanth Saripalli, Arizona State University

 

Autonomous Flight of a Samara MAV
Gerardi, Steven; Pines, Darryll; Ulrich, Evan

 

Autonomous Guidance and Control for Agile UAV Maneuvering
Singh, Leena; Yang, Lee; McConley, Marc; Appleby, Brent

 

Autonomous Helicopter R&D at the Army Aeroflightdynamics Directorate
Matthew S. Whalley, AMRDEC

 

Autonomous Helicopter Research at the Army Aeroflightdynamics Directorate
Matthew S. Whalley, AMRDEC

 

Autonomous Maneuvering of Cyclocopter using Closed-loop Motion Capture Feedback Controller
Elena Shrestha, Derrick Yeo, Vikram Hrishikeshavan, and Inderjit Chopra, University of Maryland

 

Autonomous Maneuvering of Cyclocopter using Closed-loop Motion Capture Feedback Controller
Elena Shrestha, Derrick Yeo, Vikram Hrishikeshavan, and Inderjit Chopra, University of Maryland

 

Autonomous ship board landing of a VTOL UAV
Pascual Campoy and Jose Luis Sanchez-Lopez, C.A.R. - CSIC Universidad Politecnica de Madrid, Srikant Saripalli, ASU

 

Autonomous Take-off and Landing System of the RPH 2 Unmanned Helicopter
Fuyuhiko Konnno, Akihiro Yamane, Fuji Heavy Industries Ltd.

 

Autonomous Technologies for Unmanned Aircraft Systems
Kevin Schlosser, Lockheed Martin

 

Autonomous UAV Concept for Titanic Missions
He, Chunlei; Ofoma, Uche; Wu, Chivey

 

Autonomous UAV Team Planning for Reconnaissance Missions
Garrison, D.; Szczerba, Robert; Temullo, N.

 

Autonomy - Reshaping the Vertical Lift Market
Michael Francis, Sikorsky

 

Autonomy: Technology Development for Emerging Markets
Barbara Lindauer, Sikorsky

 

Autorotation Path Planning Using Backwards Reachable Set and Optimal Control
Shane Tierney and Jack W. Langelaan, Penn State University

 

Autorotation: Building a Live Man’s Curve
José Ricardo Scarpari and João Otávio Arantes Filho, Flight Tests and Research Institute; Donizeti de Andrade, Technological Institute of Aeronautics 

 

Aviation Applied Technology Directorate Overview
Ned A. Chase, US Army

 

Aviation Applied Technology Directorate Overview
Steven Braddom, US Army

 

Aviation Diagnostic and Engine Prognostic Technology (ADEPT) for the Chinook's T-55 Engine
Kacprzynski, G.; Ling, R.; Roemer, M.; Stramiello, A.

 

Aviation Product Assessment As Viewed by the Aviation Research & Development Command
E.J. Hollman, U.S. Army Aviation Research & Development Command

 

Aviation Systems
Brian Sabourin, US Army

 

Aviation Turbine Engine Diagnostics System (ATEDS)

 

Aviation Turbine Engine Diagnostics System (ATEDS) a Maintenance Tool Designed to Reduce Repair Times & Increase Aircraft Readiness Rates
J. Moffatt, Aviation Applied Technology Directorate

 

Aviation Vibration Data
Jason Alamond, ERA Helicopters

 

Aviation Vibration Data
Jason Alamond, ERA Helicopters

 

Aviation Vibration Data Processing In Support of CBM
Danny Green, Chevron

 

Aviation Vibration Data Processing In Support of CBM
Danny Green, Chevron

 

AVIGLE -Transition Control of an Autonomous Tiltwing UAV
Tobias Ostermann, Institute of Flight System Dynamics

 

Avionic and Fire Control Equipment Complement to Enhance Attack Helicopter Survivability
E. D. Stepans, Lockheed-California Co.

 

Avionics and Electromagnetic Compatibility (EMC) Considerations on an Advanced Composite Airframe
G.W. Osborne, Bell Helicopter Textron

 

Avionics for the Light Observation Helicopter
Wilkins, F. W., Sylvania Electronics Systems

 

Avionics Systems for Helicopter Integration
D. Nelson, Collins Government Avionics Division, Rockwell International

 

Avionics Systems, Reliability, And Harsh Environments
David A. Douthit, President: Avionics Reliability

 

Avionics Troubleshooting System
M. Mastrianni, Sikorsky Aircraft Div., UTC

 

Avionics, The Key to the Future of Army Aviation
Maj. W. H. Maloney, U. S. Army CDCAA

 

Avior Overview
Kearns, Avior

 

Avoiding Controlled Flight in to Terrain (CFIT)
Reb Risty and Sandel Avionics, Sandel Avionics

 

Avoiding The Failure To Communicate
Nichols, Gregory; Price, Danon; Strauss, Nicholas; Werbos, George

 

AVX Coaxial Compound Helicopter - Configuration for Future Vertical Lift [Presentation]
Troy Gaffey, Team AVX

 

AW139 Ship Interface: Experimental Trials And Simulations
riccardo bianco mengotti and antonio la barbera and andrea ragazzi and giuseppe lo coco and federico del grande, agustawestland

 

BA609 First Flight VSTOL Handling Qualities
Fortenbaugh, Robert; Hopkins II, Roy; King, David

 

BA609 Flight Deck Design and Workload
Jeffery W. Erwin, Bell Helicopter Textron, Inc.

 

BA609 Tiltrotor Drive System
Duello, Charles

 

BA609 Tiltrotor ILS Approach Analysis And Simulation
Carl D. Griffith, Bell Helicopter Textron, Inc.

 

Back to the Future of Rotorcraft? A Bi-Rotor Configuration Whose Virtues Went Unexamined for Decades
Mullett, T.P. (Ben)

 

Background Oriented Stereoscopic Schlieren Applied to a Helicopter in Flight
H. Richard, DLR; M. Raffel, DLR; G.E.A Meier, DLR

 

BAE SYSTEMS Wind Tunnel Department STOVL Test Capabilities
Peter Palmer, BAE SYSTEMS

 

Balancing CH-53K Handling Qualities and Stability Margin Requirements in the Presence of Heavy External Loads
Cheng, R.; Faynberg, Alexander; Lavin, Mike; Pozdin, Maksym; Sahasrabudhe, Vineet; Stumm, Al; Tischler, Mark

 

Balancing Life Cycle Cost and Performance through the Product Life Cycle
Greg Kiviat, Sikorsky Aircraft

 

Balancing of High-Speed Interconnect Shafting for Operation Above Multiple Bending Critical Speeds
R. H. Badgley and J. M. Tessarzik, Mechanical Technology, Inc.

 

Ballistic Damage Tolerant Composite Flight Control Components
Maj. L. A. Fry, S. Pociluyko, Eustis Directorate, U. S. Army Air Mobility R&D Lab.

 

Ballistic Design Support Tests - A Key To Helicopter Survivability

A.C. Edwards, Hughes Helicopters

 

Ballistic Design Support Tests--A Tool for Helicopter Vulnerability Reduction
Robert E. Rohtert, Hughes Helicopters

 

Ballistic Impact Test Methodology to Document the Containment Capability of a Small Gas Turbine Engine Compressor
George Bobula and Joel Heady U.S. Army AMRDEC

 

Ballistic Impact Test Methodology to Document the Containment Capability of a Small Gas Turbine Engine Compressor
George Bobula and Joel Heady U.S. Army AMRDEC

 

Ballistic Testing Of Operating V-22 Proprotor Gearboxes
Darrell Liardon, Bell Helicopter Textron, Inc.; Alexander Bernardo, Naval Air Warfare Center; Bill Waldron, Naval Air Warfare Center

 

Ballistic Testing Of Operating V-22 Proprotor Gearboxes
Darrell Liardon, Bell Helicopter Textron, Inc.; Alexander Bernardo, Naval Air Warfare Center; Bill Waldron, Naval Air Warfare Center

 

Baseline Configuration of the CH-53K Drive System
Yuriy Gmirya, Sikorsky Aircraft Corporation; Matthew Alulis, Sikorsky Aircraft Corporation; Peter Palcic, Sikorsky Aircraft Corporation; Leslie Leigh, NAVAIRSYSCOM HQ

 

Basic Problems In Helicopter Development
F. L. Dohlhoff

 

Basic Research in Structural Dynamic System Identification
S. Hanagud, M. Meyyappa, J.I. Craig, Georgia Institute of Technology

 

Basic Theories of Fatigue Failure and Their Design Implications
Charles D. Nash, Jr.

 

Battle Damage Assessment Method for Composite Rotor Blades
Christopher Cline, The Boeing Company; john beasley, The Boeing Company; Louis Centolanza, Aviation Applied Technology Directorate

 

Bearing Fatigue and Hole Elongation in Composite Bolted Joints
Peter Grant, Nhien K. Nguyen & Adam J. Sawicki, Boeing Def & Space Group, Helicopters Division

 

Bearing Fault Diagnosis Using A Spectral Average Based Approach
David He and Brandon Van Hecke, University of Illinois-Chicago; Eric Bechhoefer, Green Power Monitoring Systems, LLC; Yongzhi Qu, The DEI Group

 

Bearing Prognostics using HUMS Condition Indicators
Bechhoefer, Eric; He, David

 

Bearing Thermal Performance and Cage Slip Measurement for All-Steel and Ceramic Hybrid Compressor Thrust Bearings
Begin, Lou; Lopez, Eleanor; Kerner, Kevin

 

Bearingless Main Rotor Whirl Test: Design, Analysis and Test Results
R.J. Murrill, B. Hamilton, V. Anand, D. Lauzon & B. Tuttle, McDonnell Douglas Helicopter Company

 

Bearingless Rotors and Higher Harmonic Control Modeling Using RACAP
K.B. Sangha, McDonnell Douglas Helicopter Co.

 

Behavior of an Extremely Flexible Rotor in Hover and Forward Flight
Sicard, Jerome; Sirohi, Jayant

 

Behavior of RTB Solutions in the Presence of Adjustment Errors
Power, Dennis; Hess, Robert

 

Being Civil in the Civil World - The Benefits of Cooperation within Our Industry
D.B. “Danny” Green, Aviation Vibration Analyst

 

Bell 412 JAR-OPS3 Approval Through Simulation and Limited Flight Testing
Corso, Lawrence; Gardos, Andrew; Morgan, Lynn; Regnier, Bradley; Schillings, John

 

Bell 412EPI Engine and Glass Cockpit Upgrade
John Schillings and Erik Oltheten and Jeff Greenwood and BJ Thomas and Hans Runge and Dale Sowers, Bell Helicopter

 

Bell 429 Handling Qualities and AFCS Flight Test Results and Pilot Evaluations
Dionne, Jacques; Emblin, Eric; Griffith, Carl; Lambert, Ed; Oltheten, Erik; Schillings, John

 

BELL 429 Main Rotor Aerodynamic and Dynamic Development
Narramore, Jim; Thomas, Brandon; Yuce, Mithat

 

Bell ACAP Full-Scale Aircraft Crash Test and KRASH Correlation
J.D. Cronkhite, Bell Helicopter Textron and L.T. Mazza, U.S. Army Aviation Applied Technology Directorate

 

Bell Commercial HUMS - Past, Present, Future
Brian Tucker, Bell Helicopter

 

Bell Commercial HUMS - Past, Present, Future
Brian Tucker, Bell Helicopter

 

Bell Eagle Eye TR-911X - Tiltrotor Unmanned Aerial Vehicle: Recent Developments, Autoland Integration, And Flight Test Demonstrations
Ben Settle, Bell Helicopter Textron, Inc.; Thomas Wise, Naval Air Systems Command

 

Bell Helicopter Business Update
Jeff Lowinger, Bell Helicopter

 

Bell Helicopter Design Visualization, More Than a Virtual Reality
Bothwell, Mike; Valentino, John

 

Bell Helicopter Textron's Applied Manufacturing Technologies for the V-22 EMD Aircraft
D. P. McIlroy, Bell Helicopter Textron, Inc.

 

Bell Knowledge-Based System Provides Producibility Analysis and Automated Tool Design for the V-22 Integrated Wiring System
Dale W. Springer, Bell Helicopter Textron, Inc.

 

Bell's Model 427 - An Affordable Light Twin Helicopter
Rodney S. Taylor, Bell Helicopter Textron, Inc.

 

BELLTECH - A Multi-Purpose Navier-Stokes Code for Rotor-Blade and Fixed-Wing Configurations
J.B. Malone and J.C. Narramore, Bell Helicopter Textron

 

Belt Mounted Airbag System for Use in Helicopter Applications
Ksiazkiewicz, Joshua; Rathmann-Ramlow, Thomas

 

Benchmarking of Obstacle Field Navigation Algorithms for Unmanned Helicopters
Goerzen, Chad; Kong, Zhaodan; Mettler, Bernie; Whalley, Matthew

 

Benchmarking of UAV Guidance Systems in Nap of the Earth (NOE) Flight
Dmitry Bershadsky and Eric Johnson, Georgia Institute of Technology

 

Bending Fatigue Strength Improvement of Carburized Aerospace Gears
A.M. Freborg, B.L. Ferguson, Z. Li, Deformation Control Technology, Inc.; D.X. Schwam, Case Western Reserve University; B.J. Smith, US Army AATD

 

Bending Strength of Spur Gear Teeth
McIntyre, W. L. and Malot, R. C., Allison (General Motors); Givens, E. R., USAAVLABS

 

Benefits Of Advanced Control Technology
Andy Handcock, GKN Westland Helicopters Ltd.; Jeremy Howitt, Defence Evaluation Research Agency; Rob Lane, GKN Westland Helicopters Ltd.; Malcolm Charlton, Defence Evaluation Research Agency; Sara Louise Johns, GKN Westland Helicopters Ltd.

 

Benefits of Early Qualification Baseline Definition in Legacy Military Rotorcraft Programs
Oxana S. Fedak, Boeing

 

Benefits of Framework Architectures in Rotorcraft
Mark Palich, Boeing; Michael Donnerstein, Boeing; Dale Johnson, AATD

 

Benefits of Virtual Testing for Drive System Development
Emmanuel Mermoz, Eurocopter

 

BERP IV - The Design, Development and Testing of an Advanced Rotor Blade
Hansford, Bob; Harrison, Robert; Stacey, Simon

 

Better Fuels – Sustainable Alternative Jet Fuel
Steve Csonka, CAAFI

 

Better Fuels – Sustainable Alternative Jet Fuel
Steve Csonka, CAAFI

 

Bicoherence Analysis for Condition Assessment of Multi-Faulted Helicopter Drivetrain Systems
Mohammed Hassan, David Coats, Yong-June Shin, Abdel Bayoumi and Alexander Barry, University of South Carolina

 

Biodynamic Model Development for Intense Shocks
Harinder J. Singh, Dr. Norman M. Wereley, University of Maryland

 

Biodynamic Response Mitigation for Seat Suspension with Adaptive Energy Absorbers
Harinder Singh, University of Maryland; Norman Wereley, University of Maryland

 

Biodynamic Response Mitigation to Shock Loads Using Magnetorheological Seat Suspensions
Choi, Y.-T.

 

Bird Dog: Coupling the Longbow Apache Attack Helicopter with an Unmanned Aerial Vehicle
Jim Kolding and Michelle Pouliot, McDonnell Douglas Helicopter Systems

 

BIRD Eco-design tool for the Aviation Industry
Ana Salles, Torsten Müller, Ann-Kathrin Wimmer Fraunhofer Institute for Chemical Technology

 

BIRD Eco-design tool for the Aviation Industry
Ana Salles, Torsten Müller, Ann-Kathrin Wimmer Fraunhofer Institute for Chemical Technology

 

Bird Impact Simulation of Polycarbonate Windshield Subject to Brittle Failures
Zi Lu and Michael Seifert and Cheng-Ho Tho, Bell Helicopter

 

Bird Strike Analysis and Test of a Spinning S-92 Tail Rotor
Alan Dobyns, Sikorsky Aircraft Corporation; Frank Federici, Sikorsky Aircraft Corporation; Robert Young, Sikorsky Aircraft Corporation

 

Bird Strike Simulation for Helicopter Rotor Blades
Cheng-Ho Tho and Michael Smith, Bell Helicopter Textron Inc., Mukesh Surana, Bell Helicopter Textron India


Abstract:

Bell Helicopter Textron is continuing to develop a bird strike simulation methodology to predict the structural responses and failure modes for both rotating and non-rotating aircraft structures using LS-DYNA®. A series of tests conducted at Southwest Research Institute (SwRI) in 2011 were used to measure bird impact loads on a Bell 429 tail rotor system. The methodology under development is used to predict the dynamic response and high speed (~550 knots) impact characteristics of the rotating tail rotor structure. The simulation is validated by comparison against measurements for pre-impact steady load, dynamic impact load, and observed structural deformation, and failure modes. 

 

BK117 C-2 Helicopter
Hiroshi Ito, Tsutomu Fujigaki, Hiroya Kato, Taihei Kaneko, Hironari Kobayashi, KHI

 

Black Hawk: A Logistic Success Story
T.M. Donahue, Sikorsky Aircraft Division, UTC

 

Blade Deflection Measurements of a Full-Scale UH-60A Rotor System
L. Olson, A. Abrego, NASA Ames Research Center; D. Barrows, NASA Langley Research Center; A. Burner, Jacobs Technology, Inc.

 

Blade Design Parameters Which Affect Helicopter Vibrations
B.P. Gupta, Hughes Helicopters, Inc

 

Blade Displacement Measurement Technique Applied to a Full-Scale Rotor Test
Anita Abrego, Lawrence Olson and Ethan Romander, NASA Ames Research Center and Danny A. Barrows and Alpheus Burner, NASA Langley Research Center

 

Blade Displacement Predictions for the Full-Scale UH-60A Airloads Rotor
Robert Biedron and Elizabeth Lee-Rausch, NASA Langley Research Center

 

Blade Flapping Motion of a Rotor Hovering above a Finite Inclined Ground Plane for Partial and Full Ground Effects Cases
Naohiro Iboshi, Noriaki Itoga, Tomoari Nagashima, Yasutaka Hayata, National Defense Academy Yokosuka; J.V.R. Prasad, Georgia Institute of Technology

 

Blade Inspection System
W.L. McKeown

 

Blade Integration of a Modular Active Trim Tab System for Onboard Rotor Tracking
Claude Matalanis, United Technologies Research Center; Andrzej Kuczek, United Technologies Research Center; Brian Wake, United Technologies Research Center; Nicholas Soldner, United Technologies Research Center; Ulf Jonsson, United Technologies Research Center; Vijaya Lakamraju, United Technologies Research Center

 

Blade Integration of a Modular Active Trim Tab System for Onboard Rotor Tracking
Claude Matalanis, United Technologies Research Center; Andrzej Kuczek, United Technologies Research Center; Brian Wake, United Technologies Research Center; Nicholas Soldner, United Technologies Research Center; Ulf Jonsson, United Technologies Research Center; Vijaya Lakamraju, United Technologies Research Center

 

Blade Motion Correlation for the Full-Scale UH-60A Airloads Rotor
Ethan Romander, Larry Meyn, Thomas R. Norman, NASA Ames Research Center; Danny Barrows, NASA Langley Research Center; Alpheus Burner, Jacobs Technology

 

Blade Motion Correlation for the Full-Scale UH-60A Airloads Rotor
Ethan Romander, Larry Meyn, Thomas R. Norman, NASA Ames Research Center; Danny Barrows, NASA Langley Research Center; Alpheus Burner, Jacobs Technology

 

Blade Mounted Devices for Tiltrotor Performance Enhancement and Noise Reduction
Todd R. Quackenbush, Daniel A. Wachspress, Robert M. McKillip, Jr, Continuum Dynamics, Inc.

 

Blade Mounted Devices for Tiltrotor Performance Enhancement and Noise Reduction
T.R. Quackenbush, D.A. Wachspress, and R.M. McKillip, Jr., Continuum Dynamics, Inc.

 

Blade Planform Optimization to Reduce HSI Noise of Helicopter in Hover
AOYAMA, Takashi; CHAE, Sanghyun; Jeong, Shinkyu; Obayashi, Shigeru; YANG, Choongmo; YEE, Kwanjung

 

Blade Property Measurement and Its Assessment on Air/Structural Loads of HART II Rotor
Brandon Hagerty, NASA Ames Research Center; Johannes Riemenschneider and Ralf Keimer, DLR (German Aerospace Center); Sung Jung and Young-Hyun You and Manoj Kumar Dhadwal, Konkuk University

 

Blade Root Integrated Fibre Bragg Grating Sensors - A Highly Redundant Data Source For Future HUMS
Manfred Hajek and Stephanie Manner and Soeren Suesse, Technische Universitaet Muenchen (TUM)

 

Blade Sections in Streamwise Oscillations into Reverse Flow
Anya Jones and Karen Mulleners, University of Maryland; Joachim Hodara and Marilyn Smith, Georgia Institute of Technology; Kenneth Granlund, Universal Technologies Corporation; Michael Ol, U.S. Air Force Research Laboratory

 

Blade Tip Aerodynamics-Profile And Planform Effects
Richard F. Spivey

 

Blade Tip Pressure Measurements Using Pressure Sensitive Paint
Oliver Wong, US Army AFDD; A. Neal Watkins and Kyle Goodman, NASA Langley Research Center; Jim Crafton, Alan Forlines and Larry Goss, Innovative Scientific Solutions, Inc. and James Gregory and Thomas Juliano, The Ohio State University

 

Blade Tip Vortex Detection in Maneuvering Flight using the Background Oriented Schlieren (BOS) Technique
Andre Bauknecht and Christoph B. Merz and Markus Raffel, German Aerospace Center (DLR), Andrin Landolt and Alexander H. Meier, ETH Zurich

 

Blade Twist - Design of Experiment
P. Nick Fletcher, Bell Helicopter Textron, Inc.

This paper was not submitted in time to be included in the printed Proceedings.

 

Blade-Vortex Interaction (BVI) Noise and Airload Prediction Using Loose Aerodynamic/Structural Coupling
B.W.-C. Sim, UC Santa Cruz/UARC; J.W. Lim, U.S. Army Aeroflightdynamics (AFDD)

 

Blade-Vortex Interaction (BVI) Noise of Helicopters Operating in Horizontal Wind Shear
Sim, Ben W.; Schmitz, Fredric H.; Beasman, T.

 

Blade-Vortex Interaction Data Obtained From A Pressure-Instrumented Model Rotor At The DNW
Peter F. Lorber, United Technologies Research Center

 

Blade-Vortex Interaction Data Obtained From A Pressure-Instrumented Model Rotor At The DNW
Peter F. Lorber, United Technologies Research Center

 

Blade-Vortex Interaction Data Obtained From A Pressure-Instrumented Model Rotor At The DNW
Peter F. Lorber, United Technologies Research Center

 

Blade-Vortex Interaction Noise of an Isolated Full-Scale XV-15 Tilt-Rotor
C. Kitaplioglu, M. Betzina, and W. Johnson, NASA Ames

 

Blade-Vortex Interaction Noise Reduction by Active Trailing-Edge Flaps
James D. Baeder, University of Maryland; Ben Wel-C. Sim, University of Maryland

 

Blade-Vortex Interaction Noise: A Comparison Of In-Flight, Full-Scale And Small-Scale Measurements
David B. Signor, Michael E. Watts, Francisco J. Hernandez, and Fort F. Felker, NASA

 

Blade-Vortex Interaction Wave Radiation Patterns of Helicopter Blades with Different Leading-Edge Geometry
Brian C. Kuo, Ben W. Sim, and Fredric H. Schmitz, University of Maryland

 

Blast Analysis of Aircraft Structure
Lisa M. Chiu, Dennis K. McCarthy, Boeing; Dr. Mark E. Robeson, U.S. Army

 

Blast Attenuating Aircraft Structure
Lisa Chiu and Dennis McCarthy, Boeing, Mark Robeson, AATD

 

Blast Fragmentation Tolerant Canopy for an AH-1W Cobra
Schadler, Jeremy; Squires, Mark

 

Blind Source Separation and Blind Equalization for Vibration Based Diagnostics of Rotorcraft Bearings
Mulugeta Haile, Anindya Ghoshal and Brian Dykas, US Army Research Laboratory

 

Blowing Flow Control of Dynamic Stall under Coupled Pitch and Freestream Oscillations
Shawn Naigle, Matthew Frankhouser, and Kyle Hird, James Gregory and Jeffrey Bons, The Ohio State University

 

Blue Edge: The Design, Development and Testing of a New Blade Concept
P. Rauch, M. Gervais, P. Cranga, A. Baud, J-F. Hirsch, A. Walter, Eurocopter; P. Beaumier, ONERA

 

Blue Pulse: Active Rotor Control at Airbus Helicopters - New EC145 Demonstrator & Flight Test Results
Antoine Rabourdin and Oliver Dieterich and Peter Konstanzer and Jean-Baptiste Maurice, Airbus Helicopters Deutschland

 

Boeing AH-64 Apache Lubrication System Cooling Development
Roy A. Bergman and Chuong Le, The Boeing Company

 

Boeing Model 347 Flying Qualities Demonstrator Program
F. H. Duke and W. E. Hooper, Boeing / Vertol

 

Boeing Rotorcraft - Riding the Wave of New Vertical Flight Technology
Chuck Allen, Boeing Rotorcraft Systems

 

Boeing Rotorcraft Mesa - 75 Years of Heritage Companies and Rotorcraft
William R. Charlton, Boeing Rotorcraft Mesa

 

Boeing Rotorcraft Systems
Phil Dunford, Boeing

 

Boeing Unmanned Airborne Systems
Jim Brooks, Boeing

 

Boeing Unmanned Little Bird Flight Test Team ? Shipboard Landing Systems Demonstration
Boeing

 

Boeing Vertol Bearingless Main Rotor Structural Design Approach Using Advanced Composites
George J. Wehnert and Marc W. Sheffler, Boeing Vertol Company; Harold K. Reddick, U.S. Army

 

Boeing Vertol Fatigue Life Methodology
George H. Thompson, Boeing Vertol

 

Boeing Vertol Fatigue Life Methodology
George H. Thompson, Boeing Vertol

 

Bonded Joint Analysis Methodology for the AH-64D Composite Main Rotor Blade
A.S. Llanos, The Boeing Company

 

Bonded Joint Technology For Composite Primary Structure
Carl Q. Rousseau, Bell Helicopter Textron, Inc.; David S. Friedmann, U. S. Army Applied Aviation Technology Directorate

 

Bonded Repair of Minimum-Gage Sandwich Structures
Joseph H. Ruddy and Anthony J. Vizzini, University of Maryland

 

Boundary Element Modeling for Delamination Analysis of Laminated Composite Structures
Makeev, Andrew; Tawfik, Samer; Tan, Xin-Yuan; Armanios, Erian A.

 

Boundary Layer Transition Detection on a Rotor Blade using Rotating Mirror Thermography
James Heineck, NASA Ames; Erich Schülein, Markus Raffel, DLR

 

Boundary Layer Transition Detection on a Rotor Blade using Rotating Mirror Thermography
James Heineck, NASA Ames; Erich Schülein, Markus Raffel, DLR

 

Boundary Layer Transition Determination for Periodic and Static Flows using Phase-Averaged Pressure Data
A.D. Gardner and K. Richter, DLR

 

Boundary Layer Transition Measurements on Hovering Helicopter Rotors by Infrared Thermography
Kai Richter and Erich Schülein, German Aerospace Center (DLR)

 

Boundary Layer Velocity Profiles on a Helicopter Rotor Blade in Hovering and Forward Flight
D. A. Blaser and H. R. Velkoff, Ohio State University

 

Bounding AoA Expectations
Michael Gaydar, NAVAIR

 

Bounding the Analysis of Alternatives
Air Platform Systems Engineering

 

Breaking the Paradigms: Catapulting STOVL
Michael M. McCrea, Francis J. O’Brimski, Peter B. Strickland, Daniel P. Raymer, Conceptual Research Corporation

 

Breaking the Paradigms: Catapulting STOVL (Brief)
Michael M. McCrea, Francis J. O’Brimski, Peter B. Strickland, Daniel P. Raymer, Conceptual Research Corporation

 

Bringing Army Helicopter Vibration Checks into the 21st Century
James L. Hunt, B. Alan Hicks, and Steven M. Krick, U.S. Army

 

Bristow: HUMS & CBM, A Large Helicopter Operator's Perspective
Rick Barnett, Bristow US LLC

 

Bristow: HUMS & CBM, A Large Helicopter Operator's Perspective
Rick Barnett, Bristow US LLC

 

British Experience of the Tropical Testing of Helicopters
G.F. Langdon, Aeroplane and Armament Experimental Establishment

 

British V/STOL Rotorcraft Concepts in the 20th Century
Hirschberg, Michael J.; M?ller, Thomas; Pryce, Michael J.

 

Brown-Out Symbology Simulation (BOSS) on the NASA Ames Vertical Motion Simulator
Albery, William; Neiswander, Gregory; Szoboszlay, Zoltan; Turpin, Terrance

 

Brownout Cloud Characterization Using the Modulation Transfer Function
John Tritschler and Roberto Celi, University of Maryland

 

Brownout Landing Aid System Technology (BLAST)
Neiswander, Gregory; Sykora, Brian; Szoboszlay, Zoltan; Turpin, Terry

 

Building Commonality Across the US Army Black Hawk Integrated Vehicle Health Management System IVHMS Fleet and Reducing Data File Size
Casey Carter, Danny Russell, Al Morris and Ron Hodgen, People Tec, Inc.; Jennifer Kerns, U.S. Army Utility Helicopter Project Office and Bill Stell, U.S. Army AMRDEC SED

 

Building Inspection Using Unmanned Vehicles
Schrage, D. P.

 

Building the Future of Vertical Lift
Nick Lappos

 

BURRO: A Servo-flap Controlled, Intermeshing Rotor VTOL UAV Demonstrator
C. T. Gunsallus and W. McAuliffe, Kaman Aerospace Corporation

 

BVI Airloads Prediction Using CFD/CSD Loose Coupling
Joon W. Lim, AMRDEC; Tor A. Nygaard, Eloret Corp. ; Roger Strawn, Mark Potsdam, AMRDEC

 

BVI Noise Control Through Feedback Based on Pressure Signals on Blade
Yasutada Tanabe, Japan Aerospace Exploration Agency; Hideaki Sugawara, Ryoyu Systems Co., Ltd.

 

BVI Noise Mitigation Via Steady Flap Deflection - An Analysis-Led Test Program
D. Wachspress, T. Quackenbush, Continuum Dynamics, Inc.

 

BVI Noise Mitigation Via Steady Flap Deflection - An Analysis-Led Test Program
D. Wachspress, T. Quackenbush, Continuum Dynamics, Inc.

 

BVI Noise Prediction Of The Split Tip Vortex Rotor Using A Time-Marching Free-Wake And Acoustic Analogy
Changjeon Hwang and Kihoon Chung, Korea Aerospace Research Institute

 

BVI Noise Prediction using a Comprehensive Rotorcraft Analysis
Daniel A. Wachspress, Continuum Dynamics, Inc.; Todd R. Quackenbush, Continuum Dynamics, Inc.

 

BVI Noise Predictions by Moving Overlapped Grid Method
Akio Ochi, Advanced Technology Institute of Commuter-Helicopter, Ltd. (ATIC); Takashi Aoyama, National Aerospace Laboratory (NAL); Shigeru Saito, National Aerospace Laboratory (NAL); Eiji Shima, Advanced Technology Institute of Commuter-Helicopter, Ltd. (ATIC); Eiichi Yamakawa, Advanced Technology Institute of Commuter-Helicopter, Ltd. (ATIC)

 

BVI Noise Reduction Research with Canard Blade Tip
Tomoki Ota, Takanori Tsukahara, and Masahiro Obukata, Fuji Heavy Industries, Ltd

 

C-gears in Rotorcraft Transmissions: a Novel Design Paradigm
Hani A. Arafa, Cairo University; Mostafa Bedewy, Cairo University, Presently at the University of Michigan

 

C-Gears in Rotorcraft Transmissions: A Novel Design Paradigm
Hani A. Arafa, Cairo University; Mostafa Bedewy, University of Michigan

 

C.R.E.A.T.I.O.N. the Onera Multi-Level Rotorcraft Concepts Evaluation Tool: The Foundations
Basset,P.-M., Tremolet, A., Cuzieux, F., Reboul, G., Costes, M., Tristrant, D., Petot D., Onera - The French Aerospace Lab

 

Cabin And Far-Field Blade-Vortex Interaction (Bvi) Noise Trends Of The MuPAL-? Research Helicopter
Ben Wel-C. Sim, Fred Schmitz, University of Maryland; Hirokazu Ishii, and Yoshinori Okuno, National Aerospace Laboratory of Japan

 

Cabin versus Far-Field Blade- Vortex Interaction Noise Level Trends
Tracy DuVall, Ben W. Sim, and Fredric H. Schmitz, University of Maryland

 

CAD-Based 3-D Structural Dynamic Modeling of the Tilt Rotor Aeroacoustic Model (TRAM) Proprotor
William Staruk, Elizabeth Weiner, Inder Chopra, University of Maryland

 

Calculated and Measured Blade Structural Response on a Full-Scale Rotor
J. Esculier, STPA, Helicopters Department and W.G. Bousman, U.S. Army Aeroflightdynamics Directorate

 

Calculating Fatigue Damage with Wireless Sensors: Duty Cycling Vs. Down Sampling
Arms, Steven; Churchill, David; Liebschutz, Daniel; Martin, Jonathan; Phan, Nam; Townsend, Christopher

 

Calculation of Dynamic Stall by Viscous-Inviscid Interaction Over Airfoils and Helicopter Blade Sections
Paul W. Von Hardenberg, Sikorsky Aircraft Corporation; Gavin A. Finn, Stone & Webster Advanced Systems Development Services, Inc.

 

Calculation of Helicopter Airfoil Characteristics for High Tip-Speed Applications
W.J. McCroskey, J.D. Baeder and J.O. Bridgeman, Aeromechanics Laboratory, AVSCOM

 

Calculation of Hub Loads at Low Airspeeds with Active Control
Kottapalli, Sesi

 

Calculation of JVX Proprotor Performance and Comparisons with Hover and High-Speed Test Data
C.W. Acree, Jr., NASA Ames

 

Calculation of Rotor Performance and Loads Under Stalled Conditions
Yeo, H.

 

Calculation of the Aerodynamic Behavior of the Tilt Rotor Aeroacoustic Model (TRAM) in the DNW
Wayne Johnson, NASA Ames Research Center

 

Calculation of Tilt Rotor Aeroacoustic Model (TRAM DNW) Performance, Airloads, and Structural Loads
Wayne Johnson, NASA Ames Research Center

 

Calculations of Quadropolar Transonic Rotor Noise Using a Formulation in the Frequency Domain
J. Prieur, ONERA

 

Calibration of a Large Ground Plane in the NASA Ames 40- by 80-Foot Wind Tunnel
Craig Hange, NASA Ames; Tom Arledge, CENTRA Technologies Inc.; Douglas Wardwell, NASA Ames; Tim Naumowicz, NASA Ames

 

Calibration of a Large Ground Plane in the NASA Ames 40- by 80-Foot Wind Tunnel (Brief)
Craig Hange, NASA Ames; Tom Arledge, CENTRA Technologies Inc.; Douglas Wardwell, NASA Ames; Tim Naumowicz, NASA Ames

 

Calibration of Airframe and Occupant Models for Two Full-Scale Rotorcraft Crash Tests
Martin Annett and Lucas Horta, NASA Langley Research Center and Michael Polanco, ATK Space Systems

 

Calibration Results of the NASA Ames Rotor Test Apparatus Steady/Dynamic Rotor Balance
Johannes M. van Aken and Randall L. Peterson, NASA Ames; Cynthia J Freedman, Sterling Federal Systems

 

Can Helicopter Rotors be Designed for Low Noise and High Performance?
D. R. Clark, Sikorsky Aircraft.

 

Can Marking Parts be Sufficient to Achieve an Enterprise UID Solution?
F. Chris Sautter, Christopher M. Goes, University of Alabama

 

Can Shock Waves on Helicopter Rotors Generate Noise? A Study of Quadrupole Source
F. Farassat, NASA Langley Research Center, and H. Tadghighi, McDonnell Douglas Helicopter Co.

 

Canadian Federal Government Aircraft Icing Research and Development Program
Peter Sully, Department of National Defence; Claude Cloutier and Mark Gauvreau, EWA-Canada, Ltd.

 

Canadian Federal Government Aircraft Icing Research and Development Program
Peter Sully, Department of National Defence; Claude Cloutier and Mark Gauvreau, EWA-Canada, Ltd.

 

Canadian High Disk-Loading V/STOL Concepts of the 20th Century
Michael J. Hirschberg and Angelo N. Collins, CENTRA Technology, Inc.; Stephen Priestley, Canadian American Strategic Review; Thomas M?ller, Aviation Historian

 

Canadian High Disk-Loading V/STOL Concepts of the 20th Century
Michael J. Hirschberg and Angelo N. Collins, CENTRA Technology, Inc.; Stephen Priestley, Canadian American Strategic Review; Thomas M?ller, Aviation Historian

 

Canadian Low Disk-Loading V/STOL Concepts of the 20th Century
Hirschberg, Mike; Mueller, Thomas; Priestley, Stephen

 

Canadian Rotorcraft: From Research to Operations
Lucie Boily, AIAC

 

Canadian Rotorcraft: From Research to Operations
Barry Kohler, Bell Helicopter Textron Canada Ltd

 

Canard Rotor/Wing (CR/W) Early History and X-50A Dragonfly Design Evolution
Charles R. Svoboda, Jr., The Boeing Co.

 

Canard Rotor/Wing (CRW) Early History & X-50A Dragonfly Design Evolution [Presentation]
Charlie Svoboda, Boeing

 

Canard Wing Concept for Compound Helicopter
Syrovy, George; Yassini, Siamak

 

Candidate Rotary-Wing Aircraft for Selected Navy/Marine Missions of the 1980s
George Unger, Naval Air Systems Command

 

Capabilities of LEWICE 1.6 and Comparison with Experimental Data
William B. Wright, NYMA, Inc.

 

Capabilities of LEWICE 1.6 and Comparison with Experimental Data
William B. Wright, NYMA, Inc.

 

Capability Driven Architecture: An Approach to Airworthy Reusable Software
Zepeda, R.; Simi, S.; Kenman, D.; Mulholland, S.; Crom, E.; Swadley, V.

 

Capability-Based Operations and Sustainment – Aviation (COST-A) Technology Development
Preston Bates, Mark Davis, James Cycon, Sikorsky Aircraft Corp; Treven Baker, Nate Bordick,  Paul Pantelis, Bruce Thompson, US Army

 

Capitalizing on Today's Technology by Using Computer Based Training/Interactive Video Disc to Enable Effective and Efficient Training to Be Conducted and Managed in the Work Place
T.C. Helmacy, Sikorsky Aircraft Division, UTC

 

Carbon Nanotube Composites- Potential for Rotorcraft Application
Koratkar, Nikhil; Proper, Andrew

 

Carbon/Epoxy Tooling Evaluation and Usage
M.D. Cimbalista, Jr., McDonnell Douglas Helicopter Co.

 

Carefree Handling and Its Applications To Military Helicopters and Missions
Major Ken Loy, USMC, Naval Air Warfare Center

 

Carefree Manoeuvring In Helicopter Flight Control
Jeremy Howitt, Defence Research Agency

This paper was not submitted in time to be included in the printed Proceedings.

 

Cargo Helicopters Mission
Paul Baker, US Army

 

Cargo Platform Maintenance Environment Design & Deployment
Beggs, Robert M.; Hoecherl, MAJ Joseph

 

Cargo Platform Maintenance Environment Design & Deployment
Beggs, Robert M.; Hoecherl, MAJ Joseph

 

Cargo Rotorcraft in Future Army Operations
G.R. Marner, Marner System Corporation; T.O. Potthoff, Army Aviation Systems Command; D.P. Schrage, Georgia Institute of Technology

 

Cargo Rotorcraft in Future Army Operations
Gene R. Marner, Marner Systems Corporation; Thomas O. Potthoff, U.S. Army Aviation Systems Command; Daniel P. Schrage, Georgia Institute of Technology

 

Cargo Unmanned Aerial System for Battlefield Logistic Support and Casualty Evacuation
Rafi Yoeli, Urban Aeronautics

 

Carmel-1

 

CarterCopter - A High Technology Gyroplane
Jay Carter, Jr., CarterCopters, L.L.C.

 

CarterCopter Technology Goes Offshore: Commercial Variant with Full Hover Capability
Jay Carter and Jeffrey Lewis, Carter Aviation Technologies

 

Case Study - Mechanistic Feed Scheduling for Multi-Axis Machining of Titanium
Harris, William

 

Case Study of Contoured Tape Laying for Production
B.J. Benda and J.P. Fleischman, Bell Helicopter Textron Inc.

 

Case Study: Zero Volatile Organic Compound Topcoat Applications - Sikorsky Helicopters
Rose, T.

 

CBM and Cost-Wise Readiness
Josh Kennedy, AMCOM IMMC

 

CBM and Cost-Wise Readiness
Josh Kennedy, AMCOM IMMC

 

CBM Component Testing at the University of South Carolina: AH-64 Tail Rotor Gearbox Studies
Nicholas Goodman, Abdel Bayoumi, Vytautas Blechertas, Ronak Shah, Yong-June Shin, University of South Carolina

 

CBM Fleet Implementation and Maintenance Decision Making Through Fatigue Life Management: Utilization and Parts Remediation Processes
Michele Kochoff Platt, AVNIK Defense; Tony M. Page, US Army AMRDEC; Deta Adams, Honeywell Aerospace; Robert E. Vaughan, US Army AMRDEC

 

CBM for Vibrating Equipment on Rotorcraft
Dr. Andrew Halfpenny, HBM; Mr. T. C. Walton, AgustaWestland

 

CBM Fundamental Research at the University of South Carolina: A Systematic Approach to U.S. Army Rotorcraft CBM and the Resulting Tangible Benefits
Vytautas Blechertasa, Abdel Bayoumia, Nicholas Goodmana, Ronak Shaha, Yong-June Shinb, University of South Carolina

 

CBM Remediation Program: Implemented Improvements and Lessons Learned
Page, Tony; Vaughan, R.

 

CBM Specialists' Meeting (Huntsville, AL, Feb. 12-13 2008)
various

 

CBM Specialists' Meeting (Huntsville, AL, Feb. 9-11 2009)
various

 

CBM Vibration Monitoring Lessons Learned from the Apache MSPU Program
Jamie Allen, U.S. Army

 

CEO Panel Discussion - Boeing
Phil Dunford, Boeing

 

CEO Panel Discussion - Eurocopter
Lutz Bertling, Eurocopter

 

CEO Straight Talk: Dunford
Dunford

 

CEO Straight Talk: Stephen C. Moss
Stephen C. Moss, AgustaWestland

 

Certification Of Composites In Civil Aircraft

R. Allen & J.R. Soderquist, FAA

 

Certification of Composites Initiative
Richard Holzwarth, Dr. Greg Schoeppner, U.S. Air Force

 

Certification of HUMS as Primary Mean for Continuing Airworthiness Process: EC225 Lessons Learned and Present Key Topics
Airbus Helicopters

 

Certification of Model 230 Helicopter for Category 'A' Elevated Helipad Operations
Joachim Goldenberg, Bell Helicopter Textron Canada; Michael Blondino and Dwayne Williams, Bell Helicopter Textron, Inc.; Leo Meslin, Bell Helicopter Textron Canada

 

Certification of the EH-101 Composite Components: A Comprehensive Approach
G. Guzzetti, U. Mariani, and F. Oggioni, Agusta S.p.A.

 

Certification Testing of a Hybrid Helicopter Airframe
R.A. Christ, McDonnell Douglas Helicopter Systems

 

Certification Tests Design Using CFD
Walter Di Bartolomeo, Peter L. Kotiuga, Pratt and Whitney Canada; Wagdi G. Habashi, CERCA

 

Certification Tests Design Using CFD
Walter Di Bartolomeo, Peter L. Kotiuga, Pratt and Whitney Canada; Wagdi G. Habashi, CERCA

 

Certification Tests of the Canadair Regional Jet for Flight in Icing Conditions
Hany Sadek, Bombardier Inc.

 

Certification Tests of the Canadair Regional Jet for Flight in Icing Conditions
Hany Sadek, Bombardier Inc.

 

Certification, Ground and Flight Testing of an Experimental IBC System for the CH-53G Helicopter
Arnold, Uwe T.P.; Strecker, Gerhard

 

CFD Analysis of High-Lift Devices on the SC-1094R8 Airfoil
EUI SUNG BAE, The Pennsylvania State University; Farhan Gandhi, The Pennsylvania State University

 

CFD and CSD Coupling Algorithms and Fluid Structure Interface for Rotorcraft Aeromechanics in Steady and Transient Flight Conditions
T.A. Nygaard, ELORET Corp.; H. Saberi, Advanced Rotorcraft Technology Inc.; R.A. Ormiston, R.C. Strawn, M. Potsdam, US Army AMRDEC

 

CFD Based Unsteady Aerodynamics For Comprehensive Rotor Aeroelastic Analysis
Jayanarayanan Sitaraman, James D. Baeder, Inderjit Chopra, University of Maryland

 

CFD Calculations on the Unsteady Aerodynamic Force of Tilt-rotor in Conversion Mode
Li Peng and Zhao Qi-Jun and Zhu Qiu-xian, National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing, China

 

CFD Calculations on the Unsteady Aerodynamic Force of Tiltrotor in Conversion Mode
Li Peng, Zhao Qi-Jun, Nanjing University of Aeronautics and Astronautics

 

CFD code validation for complete helicopters - The European GOAHEAD project
Thorsten Schwarz, DLR; Klausdieter Pahlke, DLR

 

CFD Investigation of the Helicopter-Ship Dynamic Interface
Roper, David M; Owen, Ieuan; Padfield, Gareth D.

 

CFD Investigations of 2D and 3D Dynamic Stall
A. Spentzos, G. Barakos, K. Badcock, B. Richards; Univ. of Glasgow; P. Wernert, Institut de Recherche St. Louis; S. Schrek, NREL; M. Raffel, DLR

 

CFD Method for Efficient Analysis of Flapped Rotors
R. Steijl, M. Woodgate, G. Barakos, University of Liverpool

 

CFD Modeling And Simulation For Ducted Rotor Test Stand Design
Rajneesh Singh, US Army Research Laboratory; Ross Brown, Motile Robotics Inc

 

CFD Modelling of Gas Turbine Combustor Post-Shutdown: Heat Soak-Back Phenomenon
Mohamed-Ali Ghazlani and Alain de Champlain and Bernard Paquet and Smail Kalla, Laval University; Nigel Davenport, Pratt & Whitney Canada

 

CFD Simulation of Helicopter Rotor in the Vortex Ring State Regime
Hoinville, Eric; Renaud, Thomas

 

CFD Simulation of Helicopter Tailboom Heating
R.H. Vaivads, Royal Military College of Canada; J.E.D. Gauthier, Royal Military College of Canada

 

CFD Simulations of Tiltrotor Configurations in Hover
Potsdam, Mark A.; Strawn, Roger C.

 

CFD Validation of Micro Hovering Rotor in Ground Effect
Baeder, James; Kalra, Tarandeep; Lakshminarayan, Vinod

 

CFD-CSD Analysis of Active Control of Helicopter Rotor for Performance Improvement
Jain, Rohit

 

CFD-CSD Coupled Study in the BVI Characteristics of a Saw-Tooth Blade Planform
Byung-Young Min, Lakshmi N. Sankar, Kyle Collins, Georgia Institute of Technology; Kenneth S. Brentner, The Pennsylvania State University

 

CFD/CSD Coupled Trim Solution for the Dual-Rotor CH-47 Helicopter Including Fuselage Modeling
Mahendra Bhagwat, Arsenio C.B. Dimanlig; ELORET; Hossein-Ali Saberi, Advanced Rotorcraft Technology, Inc.; Edward T. Meadowcroft, Brahmananda Panda; Roger Strawn, U.S. Army AMRDEC

 

CFD/CSD Simulation of Baseline UH-60 and Swashplateless Rotors
A. Jose, S. Ananthan, J. Baeder, University of Maryland

 

CFD/Quasi-Steady Coupling for Insects in Trimmed Forward Flight
Camli Badrya and James Baeder, University of Maryland

 

CGAD Technical Data System
D.R. Nelson, Rockwell International

 

CH - 47 Chinook From Air Assault To Desert Storm And Beyond
Charles D. Mccall

 

CH-47 Advanced Cockpit Management System
Philip L. Kirkpatrick, Charles A. DiPietro, Yongkuk Choe, Boeing Defense and Space Group

This paper was not submitted in time to be included in the printed Proceedings.

 

CH-47 Application for High Strength Alloy Steel
Mark Robuck, Patrick Darmstadt, Boeing

 

CH-47 Cargo Helicopters
Rob Barrie, Resse Hauenstein, Joe Hoecherl, US Army

 

CH-47 Helicopter Swashplate Test Stand
Daniel Bowman and Steve Fuchs, University of Dayton Research Institute and Bryan Thompson, US Army Redstone Test Center

 

CH-47D Airframe Vibration Reduction through Airframe Stiffening
Richard Gabel and Phillip Lang, Boeing Defense & Space Group, Heli Div.

 

CH-47D Tandem Rotor Outwash Survey
Mark Silva, NAVAIR; Robert Riser, NAWCAD

 

CH-53 Helicopter Night Vision System Simulation Experiments
G. Mowery & R. Milelli, Martin Marietta Corporation, L. McDonald, McDonald & Associates, C. Pentelandolfo, Naval Air Development Center, Warminster, Pa., & Lt. Col. P. Noggle, USMC, Naval Air Systems Command

 

CH-53E Digital Automatic Flight Control System
Richard D. Murphy, Sikorsky Aircraft

 

CH-53E M3M Ramp Mounted Weapon System
Archer, Anthony; Barrett, Christopher J.

 

CH-53K Control Law Risk Reduction Flight Testing on the Rascal JUH-60A In-Flight Simulator
Aaron Greenfield, Stephen Kubik, Alex Faynberg, Jonathan Litwin, Steven Marzella, Vineet Sahasrabudhe, John Rucci, Christian Corry and Steve McCulley, Sikorsky Aircraft Corp.; Ed Pavelka, Matthew Rhinehart and Sean Roark, NAVAIR and Jay Fletcher and Carl Ott, US Army RDECOM

 

CH-53K Control Laws: An Overview and Some Analytical Results
Engel, David; Faynberg, Alexander; Kubik, Stephen; Renfrow, Joseph; Sahasrabudhe, Vineet; Tonello, Oscar; Xin, Hong

 

CH-53K Control Laws: Risk Reduction Flight Testing
Vineet Sahasrabudhe, Sikorsky Aircraft Corp.; James Pritchard, NAVAIR; Arthur Gubbels, National Research Council of Canada; Alexander Faynberg, Sikorsky Aircraft Corp.; Stephen Kubik, Sikorsky Aircraft Corp.; Oscar Tonello, Sikorsky Aircraft Corp.

 

CH-53K Heavy Lift Helicopter - A Survivability Focused Design
Kathy Russell, NAVAIR; Nick Gerstner, SURVICE Engineering; Martin Krammer, NAVAIR; Richard Gardner, NAVAIR

 

CH-53K Scale Model Aerodynamic Evaluation
Bagai, Ashish; Cantono, Jeffrey; Kohlhepp, Fred; Lorber, Peter; Moffitt, Robert; O'Neill, John; Woods, Steven

 

CH47D Forward Transmission Input Pinion Seeded Fault Test
Petrella, Joseph; Kachelries, James; Neupert, Thomas

 

Challenges in Developing and Fielding an Interoperable Vehicle Health and Diagnostics System
Carter, Casey; Duke, Al; Hess, Robert; Hollon, Heather

 

Challenges In Predicting Rotor Blade Ice Protection Coverage Extent Using Alternative Flow Solver Vs Lewice2D
Roger Aubert and Jason Wright, Bell Helicopter

 

Challenges in Rotor and Hub Design for a Variable Diameter Tiltrotor
Harrington, Aaron, Milluzzo, Joseph, University of Maryland; Seshadri, Pranay; University of Cambridge; Kalra, Tarandeep and Nagaraj, VT, University of Maryland

 

Challenges in Rotor Dynamics Correlation
James M. Wang, Sikorsky Aircraft Corporation and United Technologies Corporation

 

Challenges in the Aerodynamic Optimization of High-Efficiency Proprotors
Leishman, J. Gordon; Rosen, Kenneth

 

Challenges of Flight Control in a Compound Helicopter
Fred Piasecki and Brian Geiger, Piasecki Aircraft; Joe Horn, Penn State; Paul Schifferle and Marco Lotterio, Calspan Flight Research Group

 

Challenges of Flight Control in a Compound Helicopter
Brian Geiger, Fred W. Piasecki, Piasecki Aircraft Corporation; Joseph F. Horn, The Pennsylvania State University; Marco Lotterio, Paul Schifferle, Calspan Flight Research Group

 

Challenges of Flight Control in a Compound Helicopter
Fred Piasecki, Brian Geiger, Piasecki Aircraft; Joe Horn, The Pennsylvania State University; Paul Schifferle, Marco Lotterio, Calspan Flight Research Group

 

CHAMP: A Helicopter/VTOL Flight Model for Integrated Operational Analysis
S. LaForge, J. Jennings, and A.L. Zobrist, The Rand Corporation

 

Champ: A Helicopter/VTOL Flight Model for Integrated Operational Analysis
Sally La Forge, James Jennings, and Albert Zobrist, The RAND Corporation

 

Changing Role of the Contractor Field Technical Representatives
Vincent A. Parziale, GE Aircraft Engines

 

Characteristics of Metal-Polymeric Bearings of Blade Drag Hinges, Realized on Co-Axial Helicopters
A.Z. Voronkov, N.A. Triphonova, Kamov Helicopter Scientific & Technical Co.

 

Characteristics of Tail Rotor Blade Vortex Interactions Examined using a Particle Image Velocimetry Technique
R. Green, Univ. of Glasgow; J. Early, Queens Univ.; F. Coton, Univ. of Glasgow

 

Characterization of a Millimeter-Scale Flapping Wing Driven by Two Orthogonally Oriented PZT Actuators
Christopher Kroninger, Jeffery Pulskamp, Gabriel Smith and Ronald Polcawich, US Army Research Laboratory

 

Characterization of Flexible Matrix Composite Rotorcraft Driveshafts
Shin, E.; Smith, E.; Wang, K.

 

Characterization of the Flow and Pressure Drop in Honeycomb Inlets with Grazing Flow
Bouldin, B.; Keffler, J.; Ortega, A.

 

Characterization Of Ti-6Al-4V Direct-To-Metal Fabrication Of Aerospace Grade Applications
Peter McCallum, Bell Helicopter - Textron

 

Characterization of Triaxial Braided Composite Material Properties for Impact Simulation
Arnold, William; Binienda, Wieslaw; Goldberg, Robert; Kohlman, Lee; Littell, Justin; Roberts, Gary;

 

Cheeseman Award Paper: Acoustic Flight Test of the EC130 B4 in the Scope of the FRIENDCOPTER Project
Marze, Henry; Gervais, Mark; Martin, Pierre; Dupont, Pierre

 

Cheeseman Award Paper: Consideration Of Structural Constraints In Passive Rotor Blade Design For Improved Performance
Joon Lim, US Army AFDD

 

Cheeseman Award Winning Paper: Aeroacoustic Flight Test Data Analysis and Guidelines for Noise Abatement-Procedure Design and Piloting
Spiegel, Pierre; Guntzer, Frederic; Le Duc, Anne; Buchholz, Heino

 

Chemical Ice Protection for Helicopter Rotors and a Comparison with the Electrothermal System
J. F. Van Wyckhouse

 

Chinook Cargo Helicopters
Jeff Langhout, US Army

 

CHOPPA-M: Development, Capabilities & Applications to Helicopter Operations Research
Murray Ireland, David Anderson and Douglas Thomson and Kevin Ferguson, University of Glasgow; Arvind Chandran, Gokhan Ibal, Defence Science & Technology Organisation

 

Chordwise Implementation of Pneumatic Artificial Muscles to Actuate a Trailing Edge Flap
Curt Kothera, InnoVital Systems, Inc.; Robert Vocke III and Norman Wereley, University of Maryland

 

Circulation Control Airfoils in Unsteady Flow
V. Raghavan, S.I. Pai and I. Chopra, University of Maryland

 

Circulation Control Applied To A High Speed Helicopter Rotor
Kenneth R. Reader; Joseph B. Wilkerson; David W. Taylor

 

Circulation Controlled, Fixed-Root Helicopter Concept
Gerald M. Angle II, Wade W. Huebsch, Jacky C. Prucz, James E. Smith, West Virginia University

 

Civil Aviation - National Aircraft Certification Perspectives
Morin, Transport Canada

 

Civil Certification Methods for Advanced Rotorcraft Flight Control (AFC) Systems
Robert McCallister, FAA; David King, Bell Helicopter; Ken Arifian, Sikorsky Aircraft

 

Civil Certification Methods for Advanced Rotorcraft Flight Control Systems
Arifian, Kenneth; King, David; McCallister, Robert

 

Civil Certification of a U.S. Government Procured Helicopter
J.C. Hart, Aerospatiale Helicopter Corporation

 

Civil Helicopter Operations And Regulatory Development In Thailand
Danai Lekhyananda; Srisook Chandrangsu

 

Civil Helicopter Propulsion System Reliability and Engine Monitoring Technology Assessments
J.A. Murphy, Bell Helicopter Textron and J. Zuk, Ames Research Center

 

Civil Keynote: The FAA Overview View of Health Usage Monitoring Systems
Lance Gant, FAA

 

Civil Single Pilot IFR Certification - Procedures and Pitfalls
R.D. Kimberlin, University of Tennessee Space Institute

 

Civil Tiltrotor Aircraft: A Comparison of Five Candidate Designs
J.B. Wilkerson, Boeing Helicopters and R.S. Taylor, Bell Helicopter Textron

 

Civil Tiltrotor Noise Impact Prediction Methodology
R.G. Riley, Jr., Bell Helicopter Textron, Inc.

 

Civil Tiltrotor: Flight Simulation Development of Instrument Procedures
Peter D. Klein, Bell Helicopter Textron, Inc.; Paul R. Wilkinson and Leon A. Zmroczek, Boeing Def & Space Group, Helicopter Division

 

Close Proximity Obstacle Avoidance using Sampling-Based Planners
Suresh K. Kannan, William M. Sisson, David A. Ginsberg, Jason C. Derenick, Xu Chu Ding, Thomas A. Frewen, United Technologies Research Center; Harshad Sane, Sikorsky Aircraft Corporation

 

Closed Form Solutions for Rotating Cantilever Non-uniform Raleigh Beams
Korak Sarkar and Ranjan Ganguli, Indian Institute of Science, and Isaac Elishakoff, Florida Atlantic University

 

Closed Loop Bench Testing of the Next Generation Control System for Helicopter Engines
Smith, Bert J.; Zagranski, Raymond D.

 

Closed Loop IBC-System and Flight Test Results on the CH-53G Helicopter
Auspitzer, Thomas; Fuerst, Daniel; Hausberg, Andre; Kessler, Christoph; Mueller, Matthias; Witte, Holger;

 

Closed-Loop Aeroelastic Stability Of A Hingeless Rotor Helicopter With Individual Blade Control
Marco Lovera, Patrizio Colaneri, Polytechnic University of Milan; Carlos Malpicao, Roberto Celio, University of Maryland

 

Closed-Loop Control Test of the NASA/Army/MIT Active Twist Rotor for Vibration Reduction
Cesnik, C.; Hall, S.; Shin, S.-J.

 

Closed-Loop Test of a Rotor with Individually Controlled Trailing-Edge Flaps for Vibration Reduction
Beatrice Roget and Inderjit Chopra, Alfred Gessow Rotorcraft Center

 

Closing the Gap between Capability and Affordability for System Upgrades and Major-Modifications
Sylvester Ashok, Apinut Sirirojvisuth, Georgia Institute of Technology

 

Closing the Loop on Automatic Stabilization Equipment
Walter Gerstenberger and Edward S. Carter, Jr.

 

Closing the Loop on Helicopter Crashworthiness Design Requirements
K.B. Amer, RAND Corp.

 

Co-Axial Design for Helicopter Mass Production
Watson, Rowland J., Hopp-Copters, Inc.

 

Coaxial Compound Helicopter for Confined Urban Operations
Wayne Johnson (NASA Ames Research Center), Joshua F. Elmore, Ernest B. Keen, Andrew T. Gallaher and Gerardo F. Nunez (US Army Aviation Development Directorate - AFDD)

 

Coaxial Rotor Performance and Wake Dynamics in Steady and Manoeuvring Flight
H.W. Kim, Imperial College; R.E. Brown, University of Glasgow

 

Cockpit Air Bag Systems (CABS) For Helicopters
Kazuo Katayama, Daicel Chemical Industries, Ltd.; Steve Smith, Bob Gansman, Simula Safety Systems, Inc.

 

Cockpit and Mission System Modernization
Don Anttila, Sikorsky Aircraft; Kyle DeLong, Sikorsky Aircraft; Mike Skaggs, Sikorsky Aircraft; Scott White, Rockwell Collins

 

Cockpit Design For Night Nap-Of-The Earth (Noe) Flight
John H. Emery

 

Cocured, Foam Filled Structural Component Design Considerations
J. Terceno, Sikorsky Aircraft

 

Cognitive Factors in Helicopter Low-Level Navigation: An overview of the Research
Christopher D. Wickens, University of Illinois, Aviation Research Laboratory, Verne Battiste, NASA Ames Research Center

 

Cognitive Helicopter Cockpit - From Human Operator To A Cooperation Between Man And Cognitive Assistant System
Anton Walsdorf and Reiner Onken, Bundeswehr University Munich; Jürgen Rataj, German Centre for Aerospace

 

Collaborative Autonomy for Manned/Unmanned Teams
Jameson, Steve; Franke, Jerry; Szczerba, Robert; Stockdale, Sandy

 

Collaborative Design: Human Social Practices and Computer Capabilities
Steven Poltrock and Ludwin Fuchs, The Boeing Company

 

Collaborative Investigation of the Aerodynamic Behavior of Airfoils in Reverse Flow
Joachim Hodara, Georgia Institute of Technology; Andrew Lind and Anya Jones, University of Maryland; Marilyn Smith, Georgia Institute of Technology

 

Collaborative Mapping and Search for Autonomous Helicopters
Eric Johnson and Stephen Haviland and John Mooney, Georgia Institute of Technology, Matthew White and Jonathan Hartman and Vineet Sahasrabudhe, Sikorsky Aircraft Corporation

 

Collaborative Search and Pursuit for Autonomous Helicopters
John Mooney and Eric Johnson, Georgia Institute of Technology

 

Collection and Analysis of Helicopter Combat Flight Loads Data From AH-1G Helicopters in Southeast Asia
F. J. Giessler, and J. F. Braun, Technology Inc.; and W. T. Alexander, Jr., AVLABS

 

Collective Axis Cueing and Limit Avoidance Algorithms for Carefree Maneuvering
Nilesh A. Sahani, Joseph F. Horn, Pennsylvania State University

 

Collective Limit Characterization of the CH-53D Helicopter
Frederic Neubert, USMC and Casey Gains and Emanuel Perez, NAVAIR

 

Comanche Airframe Product Development Teams - Two Years Later
Bruce F. Kay, Sikorsky Aircraft Div., UTC

 

Comanche Flight Test Simulation Station Development, Verification, and Validation Methodology
Major Timothy L. Kopra, U.S. Army Aviation Technical Test Center; Christopher C. Gayler, U.S. Army Aviation Technical Test Center

 

Comanche Helicopter in the Digital Battlefield
Donald B. Farr P.E., Boeing Helicopters Philadelphia

 

Comanche Helmet-Mounted Display Symbology Evaluation
Dowell, Susan R.; Shively, R. Jay; Szoboszlay, Zoltan P.; Turpin, Terry

 

Comanche Sensor Fusion: The Objective Force Discriminant
Maselko, William T.; Ledbetter, Paul D.; Larson, Lance P.

 

Comanche Sensor Fusion: The Objective Force Discriminant - Leveraging the Best of Pre- and Post-Declaration Information
William T. Maselko, Paul D. Ledbetter, Lance P. Larson, Northrop Grumman Electronic Systems

 

Comanche Situational Knowledge: A Consolidated Network View of the Battlefield Maximizing the Versatility of the Tass Target Threat Manager
Gustin, Jeffrey; Maselko, William

 

Comanche Warning, Caution, Advisory System - A "Display By Exception" Cockpit Philosophy.
MacIsaac, Margaret A.; Stiles, Lorren

 

Combat Maintenance and Gas Turbine Engines
D.L. Wensits, Allison Gas Turbine Div., GMC and R. Scardina, Garrett Engine Div., Allied Signal Corp.

 

Combat Operational Flight Profiles on UH-1C, AH-1G, and UH-1H Helicopters
G. L. Graham, Bell Helicopter Co.

 

Combat Simulation in the Longbow Apache Force Development Test and Experimentation (FDTE)
Scott R. Swinsick, McDonnell Douglas Helicopter Systems

 

Combat Support Requirements for Future Army Aircraft
G.L. Daugherty, Martin Marietta Orlando Aerospace

 

Combat Tempered Platform Demonstration
Marcus Cappelli, Sikorsky Aircraft; Nathaniel Bordick, U.S. Army; Jeffery Schaff and Anthony Litwinowicz, Sikorsky Aircraft

 

Combined Finite State Rotor Wake and Panel Ship Deck Models for Simulation of Helicopter Shipboard Operations
Hong Xin, Advanced Rotorcraft Technology, Inc.; Chengjian He, Advanced Rotorcraft Technology, Inc.; Johnson Lee, Advanced Rotorcraft Technology, Inc.

 

Combining Analysis and Test for Rotor Blade Development
R. Jones and N. Giansante, Kaman Aerospace Corp

 

Combining Simulink and Flightlab for Handling Qualities and Crew Station Prototyping
Borden, Christopher; Jeram, Geoffrey; Strope, Kristopher

 

Combustion-Powered Actuation for Dynamic Stall Suppression - Simulations and Low-Mach Experiments
Claude Matalanis and Byung-Young Min and Patrick Bowles and Brian Wake and Solkeun Jee, United Technologies Research Center; Tom Crittenden and Ari Glezer and George Woo, Georgia Institute of Technology

 

Command and Control of Unmanned Vehicles - Where Are We Going?
Spura, Thomas; Franke, Jerry L.; Szczerba, Robert J.; Scarangella, Mike

 

Comments on Helicopter Design and Test Requirements
Robert R. Lynn

 

Commercial "Militarization" Impact on Ballistic Tolerance
DeGarmo, Suzan

 

Commercial and Open Source Software in Rotorcraft Avionics Systems
Hrustich, John

 

Commercial CT7-8 Engine for Military Applications
M. Hughes, General Electric Aircraft Engines

 

Commercial Derivative Rotorcraft for Select DOD Missions - A Vulnerability Perspective
Michael Schuck, SURVICE Engineering Company

 

Commercial External Load Operation With the Vertol 107 Helicopter
John B. Conley, New York Airways, Inc.

 

Commercial Helicopter Operations
Flint, Knute

 

Commercial HUMS Case Studies
Murdoc Welborn and Rob Richardson, Honeywell

 

Commercial HUMS Case Studies
Murdoc Welborn and Rob Richardson, Honeywell

 

Commercial Operations and Support Savings Initiative for the OH-58D Kiowa Warrior
Kuck, Kristopher

 

Commercial School Operations
H. G. Earle

 

Commercial School Operations
H. G. Earle

 

Commercialization Initiatives in Military Engine Development/Qualification Efforts
J. L. Woracek, M. A. George, U.S. Army Aviation & Troop Command; S. W. Mitnik, AlliedSignal Engines; and A. A. Cosner, Allison Engine Co.

 

Committees, Their Importance to the Structures of the Helicopter Association International
R.D. Fox, Hillcrest Aviation

 

Common Avionics Architecture Prototype for Unmanned Aerial Systems
J.R. Moore, L.D. Olson, Rockwell Collins

 

Common Avionics Architecture System (CAAS)
LTC John Jones and MAJ Jesse Crispino, US Army

 

Common Engine Program (CEP)
Gary L. Butler, Fort Eustis

 

Common Engine Program - 3000 HP Class

 

Common Engine Program - 3000HP Class
Sandy Hoff, U.S. Army

 

Common Local Instabilities of Composite Sandwich Structures with Honeycomb Cores
Alexander Engleder and Dominik Strobel, Eurocopter Deutschland GmbH and Helmut Rapp, University of German Armed Forces

 

Community Acceptance Of Vertical Flight Vehicles
John W Leverton, Ph.D., AHS International

 

Commuter Helicopters: A Civil Reserve Resource
Morris E. Flater

 

COMOPTEVFOR
CAPT Scott F. Adley, US Navy

 

Compact Apache ECS Servicing Equipment
Beeler, Lisha Brie

 

Compact Apache ECS Servicing Equipment
Beeler, Lisha Brie

 

Compact Pericyclic Continuously Variable Speed Transmission Systems: Design Features and High-Reduction Variable Speed Case Studies
Saribay, Zihni; Smith, Edward; Lemanski, Alphonse; Bill, Robert; Wang, K.W.; Rao, Suren

 

Comparative Bench Test Assessment of Medium Authority On-blade Actuation Technologies
Curt Kothera, InnoVital Systems, Inc.; Joe Szefi, Invercon LLC; Troy Schank, Bell Helicopter

 

Comparative Numerical and Experimental Investigations of the Vortex Ring Phenomenon in Rotorcraft
Simon Newman, University of Southampton; Richard Brown, Imperial College; John Perry, Yeovil; Steven Lewis, University of Southampton; Matthew Orchard, University of Southampton; Ajay Modha, University of Southampton

 

Comparative Study Of Vibration Condition Indicators For Crack Detection In Spur Gears
Adrian Hood and Anindya Ghoshal, Army Research Laboratory, David Lewicki, NASA, Nenad Nenadic and Paul Ardis and Michael Thurston, Rochester Institute of Technology

 

Comparing Alternative Helicopter Fatigue Reliability Models
Robert Benton and Michael Kiser, US Army Aviation Engineering Directorate

 

Comparing Numerical and Experimental Results for Drag Reduction by Active Flow Control Applied to a Generic Rotorcraft Fuselage
Caroline Lienard, ONERA; Brian G. Allan, NASA; Arnaud Le Pape, ONERA; Norman W. Schaeffler, NASA

 

Comparison And Development Of Helicopter Pressure Error Correction Methods
Mark Roots, QinetiQ Ltd.

 

Comparison Between 2D and 3D Collection Efficiency Calculation
D. Guffond and R. Henry, ONERA

 

Comparison Between 2D and 3D Collection Efficiency Calculation
D. Guffond and R. Henry, ONERA

 

Comparison Between Experimental And Predicted Isolated Helicopter Rotor Transfer Functions For Unsteady Inputs On The Controls
F. Tchen Fo, ONERA; P. Eglin, Eurocopter; B. Gimonet, ALTRAN; A. Desopper, ALTRAN; S. Hellard, ALTRAN; W.v on Gruenhagen, DLR; G. Roth, Eurocopter-Deutschland

 

Comparison of a Manned Helicopter Simulation to a Computer-Based Human Performance Model
R. Jay Shively, Ames Research Center; Mark D. Burdick, San Jose State University/Ames Research Center; Michael Brickner, Pamam HFE Ltd.; Itsik Nadler, Israeli Air Force; Jacob Silbiger, Synergy Integration Ltd.

 

Comparison Of A Mechanical Fatigue Life Indicator And A Resistance Type Fatigue Life Indicator
Richard C. Rapson, Jr.; Henry R. Velkoff

 

Comparison of an Inductance In-Line Oil Debris Sensor and Magnetic Plug Oil Debris Sensor
Paula Dempsey, NASA Glenn Research Center, Roger Tuck, Jacobs Technology and Stephen Showalter, Eaton Aerospace Corporation

 

Comparison of Approximate Time Domain Aerodynamics for Flapped Airfoils with CFD Based Results with Applications
Li Liu, Peretz P. Friedmann, Ashwani K. Padthe, University of Michigan

 

Comparison of Chemical Stripping and Thermal Decomposition for the Removal of Cr-containing Coatings Present on Aircraft Al Components
J.A. Muñiz-Lerma, In-Ho Jung, M. Brochu, McGill University

 

Comparison of Chemical Stripping and Thermal Decomposition for the Removal of Cr-containing Coatings Present on Aircraft Al Components
J.A. Muñiz-Lerma, In-Ho Jung, M. Brochu, McGill University

 

Comparison of Different Approaches to Multi-Objective Parameter Optimization of Multi-Loop Flight Control Laws
Mark Tischler, US Army, Mohammadreza Mansur, U.S. Army

 

Comparison of Experimental Blade-Vortex Interaction Noise with Computational Fluid Dynamic Calculations
Megan S. McCluer and James D. Baeder; University of Maryland; Cahit Kitaplioglu, NASA Ames Research Center

 

Comparison Of Full-Scale XV-15 Blade-Vortex Interaction Noise Calculations With Wind Tunnel Data
Cahit Kitaplioglu and Wayne Johnson, NASA Ames Research Center

 

Comparison of Hard Surface and Soft Soil Impact Performance of a Crashworthy Composite Fuselage Concept
Sareen, Ashish K.; Fasanella, Edwin; Sparks, Chad; Jackson, Karen E.; Mullins, B.R., Jr.

 

Comparison of Heart and Aortic Injuries to Head, Neck, and Spine Injuries in US Army Aircraft Accidents from 1983 to 2005
Balcena, Parrish; Barth, Thomas

 

Comparison Of Helicopter Combat Environments To Structural Criteria Requirements
W. P Brown; E. P. Roeser

 

Comparison of Helicopter Copilot Workload While Using Three Navigation Systems During Nap-Of-The-Earth Flight
D. Cote, R. Simmons & G. Krueger, U.S. Army Aeromedical Research Laboratory

 

Comparison of Helicopter Rotor Propulsion Systems
Joseph Stuart III, Bell Aircraft Corp

 

Comparison of HUMS Benefits - A Readiness Approach
Hasty, Joshua; Kennedy, Josh; Speaks, Ken

 

Comparison of Measured and Predicted Noise from Interactions between Vortex and Rotor with HHC
Takashi Aoyama, Natsuki Kondo, Shigeru Saito, NAL; Takahisa Takita, Katsumi Hiraoka, Tokai University

 

Comparison of Measured Induced Velocities with Results from a Closed-Form Finite State Wake Model in Forward Flight
D.A. Peters and C.J. He, Georgia Institute of Technology

 

Comparison of Mobile Aircrew Restraint Strategies in a Full-Scale CH-46 Airframe Crash Test
Lindley Bark, NAWC-AD PAX RIVER

 

Comparison of Noise Prediction for the X-Wing System and a Conventional Rotor in Hover
R. Martin, NASA Langley Research Center

 

Comparison of Probabilistic and Fuzzy Multi-Attribute Decision Making Methods for Capturing Uncertainty in Concept Selection
Frank Patterson and Daniel Schrage, Georgia Institute of Technology

 

Comparison of Simulator Platform and Flight Tasks on Adverse Rotorcraft Pilot Coupling Prediction
Deniz Yilmaz and Marilena Pavel, Technical University of Delft; linghai lu and Michael Jump and Michael Jones, University of Liverpool

 

Comparison of SOMLA and ATB Programs for Prediction of Occupant Motions in Energy-Absorbing Seating Systems
L.W. Bark and K. Lou, Simula, Inc.

 

Comparison of Test Stand and Helicopter Oil Cooler Bearing Condition Indicators
Bolander, Nathan; Branning, Jeremy; Dempsey, Paula; Wade, Daniel

 

Comparison of Theory and Experiment for Nonlinear Flutter and Stall Response of Helicopter Blade
D.M. Tang and E.H. Dowell, Duke University

 

Comparison of XV-15 Full-Scale Wind Tunnel and In-Flight Blade-Vortex Interaction Noise
C. Kitaplioglu, M. McCluer, and C. W. Acree, Jr., NASA Ames Research Center

 

Comparison Study of Tiltrotor Whirl Flutter Using Two Rotorcraft Comprehensive Analyses
inwei Shen (University of Alabama) and Hao Kang (US Army Research Laboratory)

 

Comparisons of Predicted and Measured Rotor Performance in Vertical Climb and Descent
Fort F. Felker, NASA Ames, Robert M. McKillip, Continuum Dynamics

 

Comparisons of Predicted Brownout Dust Clouds with Photogrammetry Measurements
Monica Syal, University of Maryland, College Park; J. Gordon Leishman, University of Maryland, College Park

 

Comparisons of the Impact Responses of a 1/5-Scale Model and a Full-Scale Crashworthy Composite Fuselage Section
Fasanella, E.; Jackson, K.; Lyle, K.

 

Competing Failure Risk Assessment
Suresh Moon, L-3 Communications and Nam Phan, NAVAIR

 

Compliant Composite Part Machining
Moore, Robert

 

Component Fatigue Life Reliability with Usage Monitor
Moon, Suresh; Phan, Nam

 

Component Obsolescence Management For Rotorcraft Avionics Equipment
James W. Wasson, Smiths Industries Aerospace and Defense Systems, Inc.

 

Component Technology Insertion into Critical Avionics Applications
F. P. McCluskey, University of Maryland; D. Das, University of Maryland

 

Component Testing for the Smart Predictive System
Alex Cao and Abdel Bayoumi and Joshua Tarbutton, University of South Carolina, Lester Eisner, South Carolina National Guard

 

Component Vibration Qualification Requirements for the RAH-66 Comanche Helicopter
R. Vlaminck, Boeing Defense & Space Group, Helicopters Div. and K. Frederickson, Sikorsky Aircraft Div., UTC

 

Composite Actuators/Components for Airborne Systems
F. Ching, HR Textron Inc.

 

Composite Application for Rotorcraft Drive System Housings
Kilmain, Charles J.

 

Composite Applications in the Drive System
H. Faust and J. Mack, Boeing Vertol Co

 

Composite Bearingless Tail Rotor For Uttas
Ronald R. Fenaughty; William L. Noehren

 

Composite Cells in Aircraft Manufacturing
M. Pepka, Sikorsky Aircraft Division

 

Composite Combined Factor of Safety Which Influence Structural Design
W.S. Berczynski, Boeing Defense & Space Group, Heli Div.

 

Composite Damage Detection in Aircraft Structures Using Vibration Measurements of Modulation Under Operational Loading
Adams, Douglas; Koester, David; Jones, Chuck; Yoder, Nate; Yu, Michael; Zwink, Brandon

 

Composite Flight Service Evaluation Program For Helicopters
D.J. Baker, USA RTL Structures Lab & A.J. Gustafson, USA RTL Applied Technology Lab

 

Composite Fuselage Design Synthesis
Iqbal, Ahsan; McCarthy, D.; Walliser, Eric

 

Composite Group Technology Development
K.S. Dehoff, Boeing Helicopters

 

Composite Helicopter Tail Booms

H.J. Brown, Fiber Science, Inc.

 

Composite Inlet Housing for the T55 Engine
Barry Pickett, Mike Bielefield and Cliff Gunsallus, Kaman Aerospace Corporation; Avi Ben-Porat and Ted Westerman, Textron Lycoming

 

Composite Innovative Tooling
R.L. Metcalf and G.P. Jones, McDonnell Douglas Helicopter Co

 

Composite Landing Gear Components Made with RTM
Thuis, H.G.S.J.; Wiggenraad, J.F.M.; de Vries, H.P.J.

 

Composite Main Rotor Blade For The 214 Helicopter
R. G. Anderson; C. E. Covington

 

Composite Material Geodesic Structures - A Structural Concept for Increased Helicopter Rotor Blade Survivability
S. Pociluyko and I. E. Figge, USAAMRDL, Eustis, and C. F. Griffin and L. Blad, Lockheed-California Co.

 

Composite Ply Management
Allen E. Trudeau and Peter C. Cyr, Sikorsky Aircraft

 

Composite Rotor Hub
R.J. Mayerjak and G.T. Singley, III

 

Composite Rotor Hub, Part II
Robert J. Mayerjak, Kaman Aerospace Corporation; George T. Singley, III, AVRADCOM

 

Composite Skid Landing Gear Design Feasibility
Schrage, Daniel Schrage; Shrotri, Kshitij (Badger)

 

Composite Tension-Torsion Load Cell
Agarwal, Sandeep; Dancila, S.; Kim, I.

 

Composite Tooling for Today's Technology
Frank A. Wasilewski, Sikorsky Aircraft

 

Composite Wing Technology on the AV-8B Advanced Aircraft
Riley, B. L., McDonnell Douglas Corporation

 

Composites Qualification Criteria
David O. Adams, Sikorsky Aircraft Corporation and the Fatigue Methodology Committee of the Rotorcraft Advisory Group of the Aerospace Industries Association

 

Compound Cycle Engine Program
G.A. Bobula and W.T. Wintucky, Lewis Research Center; J.G. Castor, Garrett Turbine Engine Company

 

Compound Helicopter: Insight and Optimization
Omri Rand and Vladimir Khromov, Technion - Israel Institute of Technology

 

Compound Interest - A Dividend for the Future, Revised
D.V. Humpherson, GKN Westland Helicopters Limited

 

Comprehensive Aeromechanics Analysis of Complex Rotorcraft Using 2GCHAS
Robert A. Ormiston, Michael J. Rutkowski, Gene C. Ruzicka, ATCOM; Hossein Saberi and Yoon Jung, Advanced Rotorcraft Technology, Inc.

 

Comprehensive Aeromechanics Analysis of Complex Rotorcraft Using 2GCHAS
Robert A. Ormiston, Michael J. Rutkowski, Gene C. Ruzicka, ATCOM; Hossein Saberi and Yoon Jung, Advanced Rotorcraft Technology, Inc.

 

Comprehensive Analysis Methodology At Bell Helicopter: Copter
Jing G. Yen, John J. Corrigan, John J. Schillings, and P.Y. Hsieh, Bell Helicopter Textron, Inc.

 

Comprehensive Analysis, Prediction, and Validation of UH-60A Blade Loads in Unsteady Maneuvering Flight
Abhishek, Abhishek; Chopra, Inderjit; Datta, Anubhav

 

Comprehensive Analysis, Prediction, and Validation of UH-60A Blade Loads in Unsteady Maneuvering Flight
A. Abhishek, University of Maryland; Anubhav Datta, NASA Ames; Inderjit Chopra, University of Maryland

 

Comprehensive Modeling Approach for High-Frequency Structural Properties and Noise Transmission of Composite Panels
Abderrazak Mejdi and Bryce Gardner and Chadwyck Musser, ESI Group

 

Comprehensive Modeling Approach for High-Frequency Structural Properties and Noise Transmission of Composite Panels
Abderrazak Mejdi and Bryce Gardner and Chadwyck Musser, ESI Group

 

Comprehensive Modeling of Rotors with Trailing Edge Flaps
Friedrich K. Straub, The Boeing Company; Bruce D. Charles, The Boeing Company

 

Comprehensive Modeling of the Apache With CAMRAD II
Henry E. Jones, AMRDEC; Donald L. Kunz, Old Dominion University

 

Comprehensive Nonlinear Simulation with Robust Autonomous Control
G. Douglas Baldwin, Baldwin Technology Company, LLC

 

Comprehensive Rotorcraft Analysis for Preliminary Design and Optimization
Michael Avera, ORISE; Hao Kang and Rajneesh Singh, US Army Research Lab

 

Comprehensive UH-60 Loads Model Validation
Bauchau, Olivier; Chierichetti, Maria; McColl, Chance; Palmer, Douglas; Ruzzene, Massimo

 

Compressibility Effects on Aerodynamic Damping During Dynamic Stall Events
Patrick Bowles, Dustin Coleman, Thomas Corke and Flint Thomas, University of Notre Dame and Mark Wasikowski, Bell Helicopter Textron

 

Compressible Dynamic Stall Mechanisms Due to Airfoil Pitching and Freestream Mach Oscillations
Kyle Gompertz, Christopher Jensen, James Gregory and Jeffrey Bons, The Ohio State University

 

Compressible Dynamic Stall of an SSC-A09 Airfoil Subjected to Coupled Pitch and Freestream Mach Oscillations
James Gregory and Jeffrey Bons and Kyle Hird and Matthew Frankhouser, The Ohio State University

 

Compression Molding of Composite Tailboom Frames
Ali Yousefpour and Steven Roy, National Research Council Canada; Pierre Beaulieu and Felix Bednar, Bell Helicopter Textron Canada Ltd.

 

Compression Strength Prediction of Impact-Damaged Composite Sandwich Panels
Jackson, Wade; Ratcliffe, James; Schaff, Jeff

 

Compressive Failure Mechanisms in Composite Sandwich Structures
Michael K. Cvitkovich, NASA Langley Research Center; Wade C. Jackson, NASA Langley Research Center

 

Compressor Study to Meet Large Civil Tilt Rotor Engine Requirements
Veres, Joseph

 

Compromises Associated With VTOL and STOL Propellers
Robert A. Rogers

 

Computation and Measurement of the Flowfield Near a Swept Rotor Blade Tip in Hover
F.L. Tsung, S.G. Liou, N.M. Komerath, and L.N. Sankar, Georgia Institute of Technology

 

Computation and Measurement of the Flowfield Near a Swept Rotor Blade Tip in Hover
Tsung, Fu-Lin, Liou, Shiuh-Guang, Komerath, Narayanan, M., Sankar, Lakshmi N., Georgia Institute of Technology

 

Computation of Loads on the McDonnell Douglas Advanced Bearingless Rotor
Khanh. Nguyen, NASA Ames Research Center; Dan Lauzon. Vaidyanathan Anand, McDonnell Douglas Helicopter Systems

 

Computation of the BVI Noise for the BO 105 Model Rotor in Forward Flight and Comparison with Wind-Tunnel Tests
M. Schaffar, J. Haertig and P. Gnemmi, Institut Franco-Allemand de Recherches de Saint-Louis

 

Computation of UH-60A Airloads Using CFD/CSD Coupling On Unstructured Meshes
Robert Biedron, NASA Langley Research Center; Elizabeth Lee-Rausch, NASA Langley Research Center

 

Computational Aero-acoustic Analysis and Flight Test of UH-60 for Hover
Nameun Park, Chulhun Woo, Jhageun Park, Gunmook Choi, Korea Aerospace Industries(Ltd.)

 

Computational Aeroacoustic Study of Isolated Blade-Vortex Interaction Noise
James D. Baeder, University of Maryland; G.R. Srinivasan, JAI Associates, Inc.

 

Computational Aeroelasticity of Rotating Wings with Deformable Airfoils
Cesnik, Carlos; Cook, James; Smith, Marilyn; Thepvongs, Smith

 

Computational Analysis of a Microtab-Based Aerodynamic Load Control System for Rotor Blades
K. Standish, C. van Dam, UC Davis

 

Computational Assessment of the Aerodynamic Performance of a Variable-Speed Power Turbine for Large Civil Tilt-Rotor Application
Gerard Welch, NASA Glenn Research Center

 

Computational Evaluation of Directed Synthetic Jets for Dynamic Stall Control
Brian E. Wake, United Technologies Research Center; Elizabeth A. Lurie, United Technologies Research Center

 

Computational Fluid Dynamics Analysis of a Coaxial Rotor Using Overset Grids
Gene C. Ruzicka and Roger C. Strawn, AMRDEC

 

Computational Investigation and Fundamental Understanding of a Slowed UH-60A Rotor at High Advance Ratios
Mark Potsdam, US Army AFDD (AMRDEC) and Anubhav Datta and Buvana Jayaraman, Science and Technology Corp.

 

Computational Investigation Of Coaxial Rotor Aerodynamics In Hover
Vinod K. Lakshminarayan, University of Maryland; Karthikeyan Duraisamy, University of Glasgow; James D. Baeder, University of Maryland

 

Computational Investigation of Micro-Scale Shrouded Rotor Aerodynamics in Hover
V. Lakshminarayan, J. Baeder, University of Maryland

 

Computational Modeling of Diving-turn Maneuvers Using a Hybrid Methodology
Ritu Marpu and Lakshmi Sankar, Georgia Institute of Technology; Steve Makinen, Sikorsky Aircraft Corporation and James Baeder, University of Maryland

 

Computational Modeling of Hovering Rotor and Wake Aerodynamics
Roger C. Strawn, Ames Research Center; M. Jahed Djomehri, Ames Research Center

 

Computational Procedures for the Aeroelastic Simulation of Maneuvering Rotorcraft Vehicles
Bottasso, Carlo L.; Croce, Alessandro; Leonello, Domenico; Riviello, Luca

 

Computational Simulation and Analysis of Bell/Boeing Quad Tiltrotor Aero Interaction Using a Navier-Stoke Flow Solver
Narramore, Jim; Sheng, Chunhua

 

Computational Studies of the Effects of Gurney Flaps on Autorotative Performance of Rotors in Descent Flight
Byung-Young Min, Lakshmi N. Sankar, and Chanin Tongchitpakdee, Georgia Tech; Yung H. Yu, Konkuk University

 

Computational Study of Flow Interactions in Coaxial Rotors
Seokkwan Yoon, Henry C. Lee, and Thomas H. Pulliam (NASA Ames Research Center)

 

Computational Study of the Roles of Shrouds and Multiphase Flow in High Speed Gear Windage Loss
Robert Kunz, Kerrie Schmehl and Sean McIntyre, The Pennsylvania State University and Matthew Hill, Bell Helicopter Textron

 

Computational Study of Wind Turbine Performance and Loading Response to Turbulent Inflow Conditions
Jay Sitaraman and Beatrice Roget and Christopher Gundling, University of Wyoming, Pierangelo Masarati, Politechnico Di Milano

 

Computational Techniques for Improved Blade Vortex Interaction Modeling
Devon S. Prichard and D. Douglas Boyd, Jr., Lockheed Engineering and Sciences Co.; Casey L. Burley, NASA Langley Research Center

 

Computational/Experimental Study of Hovering Rotor Tip Vortex Formation
K. Duraisamy, M. Ramasamy, J.D. Baeder, J.G. Leishman, University of Maryland

 

Computational Modeling of the CH­-47 Helicopter in Hover
Arsenio C.B. Dimanlig, NASA­ Ames; Edward T. Meadowcroft, Boeing; Roger Strawn and Mark Potsdam, U.S. Army

 

Computations and Experiments on Flow Physics of Edgewise Ducted Fan Air Vehicles
Jason Halwick, James Dreyer, Jules Lindau and Dennis McLaughlin, The Pennsylvania State University

 

Computations of Dynamic Stall Control with Combustion-Powered Actuation
Solkeun Jee, Claude Matalanis, Byung-Young Min, Patrick Bowles, Brian Wake, United Technologies Research Center; Thomas Crittenden and Ari Glezer, Georgia Institute of Technology

 

Computed Induced Velocity, Induced Drag, and Angle of Attack Distributions for a Two-Bladed Rotor
Raymond Piziali and Frank DuWaldt, Cornell Aeronautical Laboratory

 

Computer Aided Coordinate Measuring Systems
J.W. Nastri, Sikorsky Aircraft Div., UTC

 

Computer Aided Coordinate Measuring Systems
J.W. Nastri, Sikorsky Aircraft Div., UTC

 

Computer Aided Helicopter Design
H. Rosenstein & K. Stanzione, Boeing Vertol Company

 

Computer Aided Non Destructive Inspection and Disposition (CANDID): Overview and Benefits of Automating NDI of Rotorcraft
Steve P. Hazen, The Boeing Company

 

Computer Aided Process Planning
R.C. Read, Jr.

 

Computer Assisted High Speed Balancing Of T53 And T55 Power Turbines

T.J. pojeta, US Army AVRADCOM & T.J. Walter, Mechanical Technology, Inc.

 

Computer Flight Testing Of Rotorcraft
John J. Corrigan, Bell Helicopter Textron, Inc.; Austin Meyer, Laminar Research; Michael Bothwell, Hiram Brown, Bell Helicopter Textron, Inc.

 

Computer Graphics Used in Numerical Control Programming
Richard N. Hayes, Sikorsky

 

Computer Simulation and Modeling - A Tool for Inventory Management
J.G. Williams, Bell Helicopter Textron

 

Computer Visualization Of Vortex Wake Systems
Roger C. Strawn, Ames Research Center; David N. Kenwright, NASA Ames Research Center; Jasim Ahmad, NASA Ames Research Center

 

Computerized Aerodynamic Design of a Transonically "Quiet" Blade
M.E. Tauber, NASA Ames Research Center

 

Computerized Gear Grinding System Development
F.Z. Marcenaro, Bell Helicopter Textron

 

Computerized Three-Dimensional Aerodynamic Design of a Lifting Rotor Blade
M.E. Tauber & R.M. Hicks, NASA/Ames Research Center

 

Computing Industry Applications to Rotorcraft Avionics
Andrew Augenstein and Mark Hansen, Boeing

 

Concept Demonstration of Automatic Subsystem Parameter Monitoring
R.V. Kurowsky, U.S. Army, AVRADA and M.S. Randolph, General Electric Company

 

Concept Feasibility Demonstration for the Army Cockpit Delethalization Program
R.L. Greth, W.B. Shope, and M.S. Pfaff, LME, Inc. and K.F. Smith, Aviation Applied Technology Directorate

 

Concept of a Predictive Analysis Tool for Ship Helicopter Operational Limitations of Various In-Service Conditions
Alrik Hoencamp, Royal Netherlands Navy

 

Concept Selection and Analysis of Large Wind Generator Systems
Richard C. Meier, Kaman Aerospace Corp.

 

Concepts and Requirements Directorate Mission
Glenn D. Harrison, US Army

 

Concepts and Techniques for Helicopter Airframe Fatigue Tests
Walter A. Lane, Sikorsky Aircraft Div.

 

Concepts for Certifying a Data-Driven HUM System
Hiatt, Daniel S.; Hayden, Rex

 

Concepts for Multi-Speed Rotorcraft Drive System
Handschuh, Robert; Lewicki, David; Stevens, Mark

 

Concepts for Multi-Speed Rotorcraft Drive System - Status of Design and Testing at NASA GRC
Mark Stevens and David Lewicki, NASA John H. Glenn Research Center; Robert Handschuh, NASA

 

Concepts for Reapplying HUMS Technology Across Rotorcraft Platforms
Robert Hess, BFGoodrich Aerospace; Douglas Patriquin, BFGoodrich Aerospace

 

Conceptual Aircraft Design - Lost Art or Science?
S. B. Wilson, DARPA; Leo Fila, CENTRA Technology

 

Conceptual Design and Performance Analysis for a Large Civil Compound Helicopter
Russell, Carl and Johnson, Wayne, NASA

 

Conceptual Design Aspects of Three General Sub-Classes of Multi-Rotor Configurations: Distributed, Modular, and Heterogeneous
Larry A. Young, NASA

 

Conceptual Design of a Ducted Fan?Based Vertical Takeoff and Landing Tactical Unmanned Aerial Vehicle
Jonathan D. Keith, Empirical Systems Aerospace, LLC; Ryan S. Wood, Frontline Aerospace, Inc.

 

Conceptual Design Of A High-Speed Variable Configuration Compound Helicopter