2D Polar Assessment in Icing Wind Tunnel for iced Helicopter Blade Profiles
3-D Steady-State Wall Heat Fluxes and Thermal Analysis of a Stratified-Charge Rotary Engine
20-Hour Follow-on Flight Test Program, XV-9A Hot Cycle Research Aircraft
28VDC Brushless Starter Generator Technology
72 Curved Fin Rotor Design Reduces Maximum Rotor Temperature
72 Curved Fins and Air Director Idea Increases Airflow through Brake Rotors
270 Volt Direct Current Generating System: Design, Development and Test
A 5 Phase Brake Insulator Engineering Selection Process
ACCELERATED SERVICE TESTING OF TURBO-PROP ENGINES IN USAF TEST BED AIRCRAFT
A CFD Approach for Predicting 3D Ice Accretion on Aircraft
A Comparative Study of Four Algebraic Transition Models
A Comparison by Thermal Analysis of Rotor Alloys for Automobile Disc Brakes
A Comparison of Optimal and Noise-Abatement Trajectories of a Tilt-Rotor Aircraft