A coupled aero-structural optimization method for complete aircraft configurations
A Coupled Aero-Structural Optimization Method for Complete Aircraft Configurations
Acoustical Excitation of Burning Fuel Droplets in Normal Gravity and Microgravity
Acoustically Driven Droplet Combustion with Alternative Liquid Fuels
Active Multiple Winglets for Improved Unmanned-Aerial-Vehicle Performance
ACTIVE VEHICLE SEAT WITH SPRING-SUPPORTED MORPHING PORTIONS
Activities, accessibility and mobility for individuals and households
Actuator Bonding Optimization and System Control of a Rotor Blade Ultrasonic Deicing System