Testing of Compact Inflatable Wings for Small Autonomous Aircraft
Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing
Development of a Novel Low Stored Volume High-Altitude Wing Design
AIAA-2006-1697 Development of a Finite Element Model of Warping Inflatable Wings
AIAA-2006-1696 A High-Altitude Test of Inflatable Wings for Low-Density Flight Applications