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title: Aircraft Aerodynamic Design
Workstation for the integrated design and simulation of flight control systems
Voltage doubling rectifier for electric aerodynamic propulsion high-voltage power supply
Versatile, modular, extensible vtol aerial platform with autonomous flight mode transitions
Variable structure robust flight control system for the F-14
Tracked Air Cushion Research Vehicle. Volume III Research Vehicle Research Plan
Towards Complete Configurations Using an Embedded Grid Approach
Towards bio-inspired structural design of a 3D printable, ballistically deployable, multi-rotor UAV
The SOFIA aircraft and its modification
Thermal management of military fighter aircraft electro-optics pod: an invited paper
The Development of a Small Solar Powered Electric Unmanned Aerial Vehicle Systems
The Development of a Small Solar Powered Electric Unmanned Aerial Vehicle Systems
Summary of Rotochute Development
Special problems associated with aircraft radomes
Simulation based aerodynamic design
Screening and shielding in aircraft - the balanced approach
Sabot High Speed Interceptor AE 4273 Aircraft Design
QFT force loop design for the aerodynamic load simulator
Performance Trade-offs and Operations of Electric Boosted Aircraft for 2030 Single-Aisle Market