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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
- > Tracking Pitch Link Dynamic Loads with Energy Harvesting Wireless Sensors
- > Sinusoidal Gust Response of RC Propellers in Tandem Configuration
- > A Practical Approach to Obstacle Field Route Planning for Unmanned Rotorcraft
- > Design Parameters for Coaxial Rotary Wing MAVs with Passive Roll and Pitch Stability
- > The Application Of Process Simulation Tools To Reduce Risks In Liquid Molding Of Composites
- > Design and Preliminary Flight Test of a 35 GHz Forward-Looking Collision Avoidance Radar
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