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- > A Comparison of Two Alternative Velocity Vector Cue Combinations for the AH-64D Integrated Helmet and Display Sight Subsystem
- > Effects of Surface Blowing/Suction on the Aerodynamics of Helicopter Rotor Blade-Vortex Interaction (BVI) - A Numerical Simulation
- > The Use of GPS Tracking and Guidance Systems for the Chicken Little Joint Project's "Acoustic Week" Flight Test Program
- > High-Speed Vertical Takeoff and Landing (HSVTOL) Aircraft - Arion
- > Determination of AH-64 Airframe In-Flight Modal Frequencies Using Rotor Control-Induced Excitations
- > Vertical Motion Simulator Handling Qualities Testing of a Piloted eVTOL Vehicle Having a Degraded Powertrain
- > Development of a Novel High Authority Piezoelectric Actuator for Rotor Blades with Trailing Edge Flaps
- > Natural Fatigue Crack Initiation and Detection in High Quality Spur Gears
- > Prediction and Measurement of the Deformations of an Extremely Flexible Rotor Using Digital Image Correlation
- > Investigation of Maximum Blade Loading Capability of Lift-Offset Rotors
- > Optimum Performance Of An Actuator Disk By A Compact Momentum Theory Including Swirl
- > Design Aspects of the PZL SW-4 Helicopter Structure
- > The Effects of Crosswind Flight on Rotor Harmonic Noise Radiation
- > Initial Tiltrotor Aeroacoustic Code (TRAC) Predictions For The XV-15 Flight Vehicle And Comparison With Flight Measurements
- > Dynamic Behavior and Passive Vibration Control of a Flexible Tip-Loaded Support Arm System with Bracing Struts and Tailored Particle Impact Dampers
- > Model-Based Design and Integrated Manufacturing of the Sikorsky UH-60 Blackhawk Composite Tailcone
- > Quantitative Method for the Evaluation of Pilots’ Performance to Enhance Training in Flight Simulators Applied to Vortex Ring State (VRS) Recovery Maneuvers
- > The Methodology And Economics Of Technological Upgrade Demonstrated By The SH-2F To SH-2G Conversion Program
- > German V/STOL Rotorcraft And Propellercraft In The Twentieth Century
- > New Methods For Rotor Tracking And Balance Tuning And Defect Detection Applied To Eurocopter Products
- > Adding Realism to Inverse Simulation of Helicopters in Aggressive Maneuvering Flight Using a Receding Horizon Approach
- > Crack Propagation Test And Analyses Of CH-47 Swashplate Rotating Ring
- > Experimental Whirl Tower Tests Approaching and Surpassing Stall for a Variety of Tip Speeds
- > Simulation and Analysis of NASA Lift Plus Cruise eVTOL Crash Test
- > Design and Certification of the K-MAX Helicopter External Personnel Carrying Device System
- > Identification Modeling and Analysis of the Coupled Drive-Train/Inflow in Miniature Rotorcraft Axial Flight Dynamics
- > Analysis and Tests of Reinforced Carbon-Epoxy/Foam-Core Sandwich Panels with Cutouts
- > Development Of The V-22 Drive System Vibration Monitoring - An Update
- > Cost And Weight Optimization Of A Hybrid Composite/Metallic Light Helicopter Fuselage Design
- > Automated Helicopter Vibration Diagnostics for the US Army and National Guard
- > Control and Stability Characteristics of Gamera II: a Human Powered Helicopter
- > Computational Acoustic Prediction on the Aerodynamic and Acoustic Rotorprop Test
- > Effects of Gas Turbine Component Performance on Engine and Rotary Wing Vehicle Size and Performance
- > A Method of Qualitative Analysis During Conceptual Design as Applied to Unmanned Aerial Vehicles
- > Correlation Between Stress Pattern Analysis by Thermal Emission (SPATE) Test and Finite-Element Modeling (FEM) for the AH-1W Tailboom
- > Flight Dynamics Of An Articulated Rotor Helicopter With An External Slung Load
- > Performance Impacts of Wing and Rotor Placement on a Quadrotor Tailsitter
- > A Framework for Cost-Benefit Analysis of Tiltrotor Aircraft
- > Lightning Strike Experiments and Their Direct Effects on Flax Fiber-Reinforced Polymer Panels for Rotorcraft Components
- > Application of MADYMO to Helicopter Energy-Absorbing Seat/Occupant System Analysis
- > Correlation of UMARC Predictive Capability of Three Slowed Rotor Experiments at High Advance Ratios
- > CBM Component Testing At The University Of South Carolina: AH-64 Gearbox Grease Studies
- > The Technical Legacy of Prof. Howard C. “Pat” Curtiss, Jr.
- > Robust Stability Analysis: A Tool to Assess the Impact of Biodynamic Feedthrough on Rotorcraft
- > Validation of Concepts for Improved Occupant Crash Safety in Helicopters
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