Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing
Experimental Characterization of Hydrocarbon-Fueled, Axisymmetric, Scramjet Combustor Flowpaths
Modeling and Characterization of Damage Processes in Metallic Materials
Development of a Novel Low Stored Volume High-Altitude Wing Design
VORTEX MACHINING: LOCALIZED SURFACE MODIFICATION USING AN OSCILLATING FIBER PROBE
Testing of Compact Inflatable Wings for Small Autonomous Aircraft
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
AIAA-2006-1805 Measurement of In-Plane Motion of Thin-Film Structures Using Videogrammetry
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
AIAA-2004-1503 Development of UV-Curable Inflatable Wings for Low-Density Flight Applications
Experimental Results Regarding Two-Dimensional Deployment of Inflatable Beams
Modeling the Dynamics of Large Diameter Doubly Curved Shells made from Thin-Films
SPICE modeling of ferroelectric liquid crystal on silicon microdisplays [5181-21]
The application of finite element modelling to guided ultrasonic waves in rails