Part-Task Simulator for Truck Transmission Gear Shifting
Effect of Real and Simulated Space Flight on Collagen Crosslink Excretion
Simulation of Deployment Dynamics of an Inflatable Solar Array
Post-Flight Testing and Analysis of Zero-G Foam Rigidized Struts
A Pressurized Deployment Model for Inflatable Space Structures
AIAA-2001-1264 Experimental Results Regarding the Inflation of Unfolding Cylindrical Tubes
A Reusable Space Vehicle Design Study Exploring Sharp Leading Edges
Low Speed Aerodynamics and Landing Characteristics of Sharp-Class Crew Transfer Vehicle Concepts
Staged Microgravity Deployment of a Pressurizing Scale Model Spacecraft
Experimental Results Regarding Two-Dimensional Deployment of Inflatable Beams
Recent Results on Liquid Fuelled APU for Truck Application
SPICE modeling of ferroelectric liquid crystal on silicon microdisplays [5181-21]
AIAA-2004-1503 Development of UV-Curable Inflatable Wings for Low-Density Flight Applications
AIAA-2004-6570 Flying on Air: UAV Flight Testing with Inflatable Wing Technology
Development and Flight Testing of a UAV with Inflatable-Rigidizable Wings
A Preliminary Evaluation of Child Restraints and Anchorage Systems for an Australian Car
BIG BLUE II: Mars Aircraft Prototype with Inflatable-Rigidizable Wings
Design and Flight Testing of Inflatable Wings with Wing Warping
AIAA-2006-1805 Measurement of In-Plane Motion of Thin-Film Structures Using Videogrammetry
Electrical System Evaluation Platform for Uninhabited Autonomous Vehicles
AIAA-2006-1697 Development of a Finite Element Model of Warping Inflatable Wings
Flight Control of a UAV with Inflatable Wings with Wing Warping
AIAA-2006-1696 A High-Altitude Test of Inflatable Wings for Low-Density Flight Applications
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing AIAA Paper
Flight Testing and Simulation of a Mars Aircraft Design Using Inflatable Wings AIAA Paper
Altitude Comparison Technique Using the MC-130H APN-232 RADAR Altimeter
Testing of Compact Inflatable Wings for Small Autonomous Aircraft
2008-01-0777 Experimental Validation of a Coupled Fluid-Multibody Dynamics Model for Tanker Trucks
Development of a Novel Low Stored Volume High-Altitude Wing Design
Design Limitations of Deployable Wings for Small Low Altitude UAVS
Design Limitations of Deployable Wings for Small Low Altitude UAVs
Modeling and Characterization of Damage Processes in Metallic Materials
Modeling and Characterization of Damage Processes in Metallic Materials