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- > Evaluation of Material Models Within LS-DYNA for a Kevlar/Epoxy Composite Honeycomb
- > CFD-CSD Coupled Study in the BVI Characteristics of a Saw-Tooth Blade Planform
- > Lubricant Condition Assessment System (LUCAS), an Enabler for Condition Based Maintenance Best Practice
- > Estimating Blade Section Airloads from Blade Leading-Edge Pressure Measurements
- > Turbulence Modifications and Phase Couplings in Ground Effect under Simulated Brownout Conditions
- > Introduction to the US Army PEO Aviation (PEO AVN) Enterprise Architecture Framework (EAF)
- > Determination of The Maximum Service Temperature for Composite Main Rotor Blade
- > Operational Durability of Thermoplastic Composites in Primary Aircraft Structure
- > Comparison of HUMS Benefits - A Readiness Approach
- > Canadian Rotorcraft: From Research to Operations
- > DoD Helicopter Mishaps FY85-05: Findings and Recommendations
- > Double Fourier Applications for Real Time Aerodynamic Load Recovery
- > Computational Aeroelasticity of Rotating Wings with Deformable Airfoils
- > Understanding UAS Operator and Aviation Authority Challenges with the SORA Process for UAS Operational Approval in DACH Nations
- > HUMS for Light Helicopters in Rescue and EMS Operations
- > Fatigue Characteristics Of S-2 Glass/Epoxy Composites
- > Analysis of Magnetic Communications for Use on Rotorcraft
- > Correlation of V-22 Dynamic Loads Model to V-22 Aircraft Drop Test
- > The FW-61, Henrich Focke's Masterpiece
- > Structural Optimisation and Aeroelastic Tailoring of the BERP IV Demonstrator Blade
- > Digital Open-Architecture Inter-Communications Systems (ICS) for the Expanding Requirements of Rotary Wing Operations
- > System Identification of a Free-Flying Quadrotor in a Wind Tunnel using Motion Capture Feedback
- > Influence of Wing-Propeller Aerodynamic Interactions on Aeroelastic Damping
- > Design of the Facility for Outdoor Rotor Testing
- > Optimization and Piloted Simulation Results of the AH-64D Modern Control Laws
- > Noise Certification of the MD900 Explorer Helicopter
- > Magnesium: The Rotorcraft Designer's Dilemma
- > A Retrospective Survey of Pilot-Structural Coupling Instabilities in Naval Rotorcraft
- > Analysis of a Helicopter Tail Landing Gear System Featuring Electrorheological Fluids
- > An Integrated Approach to Rotorcraft Total Survivability and Operational Durability
- > Modeling and Flight Dynamics Analysis of Rotor-on-Wing Interference Effects of a Winged Single Main Rotor
- > V-22 EMD Cockpit and Full Fidelity Simulation: The Path to Operational Suitability
- > Aerodynamic Studies of High Advance Ratio Rotor Systems
- > Ground Effect of a Rotor Hovering above a Confined Area
- > Torque Sensor Validation and Signal Recovery for Turboshaft Engines
- > Forward-Looking Integrated Symbology for 4-D Re-Routable Helicopter Approach-To-Landing
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