SAE Aero Design East: BYU-Idaho Aero Team 326 – Final Report Document
New Guidelines for Implementation of Structural Health Monitoring in Aerospace Applications
SUAV: Project Case Study to Integrate a Tubular Solid Oxide Fuel Cell Hybrid System into a Small UAV
Aircraft Flashtube Anticollision Lighting Systems
Concept Development of a Pneumatically Driven, Fixed Root Circulation Controlled Helicopter
Further Evaluation of Scaling Methods for Rotorcraft Icing
Aircraft Wing Build Philosophy Change through System Pre-Equipping of Major Components
Aircraft Engine Attachment and Vibration Control
Lighting, Aircraft Interior, Installation of
NASA Heavy Lift Rotorcraft Systems Investigation
Safety Assessment of General Aviation Airplanes and Rotorcraft in Commercial Service
Aircraft Flexible Tanks General Design and Installation Recommendations
Crashworthy Landing Gear Design
Aerodynamic Analysis of the Elytron 2S Experimental Tiltwing Aircraft