PREPARATION OF THE KENTUCKY RE-ENTRY UNIVERSAL PAYLOAD SYSTEM FOR ORBITAL FLIGHT
Effect of Boundary Conditions on Geometric Control for an Inflatable Pathfinder System
Experimental Analysis of Carbon Nitridation and Oxidation Efficiency with Laser-Induced Fluorescence
Designing Collaborative Automated Planners for Agile Adaptation to Dynamic Change
2012-01-1092 Electrically Heated Catalysts for Cold-Start Emissions in Diesel Aftertreatment
Electrically Heated Catalysts for Cold-Start Emissions in Diesel Aftertreatment
Exploration of Aerated-Liquid Jets Using X-Ray Radiography
Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing
INCORPORATING THROUGH LIFE SUPPORT REQUIREMENTS INTO SUBMARINE DESIG
Experimental Characterization of Hydrocarbon-Fueled, Axisymmetric, Scramjet Combustor Flowpaths
Modeling and Characterization of Damage Processes in Metallic Materials
ADVANCED MULTIDISCIPLINARY OPTIMIZATION TECHNIQUES FOR EFFICIENT SUBSONIC AIRCRAFT DESIGN
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
High-Altitude LTA Airship Efforts at the U.S. Army SMDC/ARSTRAT
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
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
A New Model to Improve Aggregate Air Traffic Demand Predictions AIAA Paper
Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing AIAA Paper
Landing Gear Mass Prediction - A Combined Analytic and Parametric Approach
ELECTRICAL ARC IGNITION TESTING OF SPACESUIT MATERIALS
Flight Testing and Simulation of a Mars Aircraft Design Using Inflatable Wings AIAA Paper
Performance of Booster Seats in Side Impacts: Effect of Adjacent Passengers and ISOFIX Attachment
Flight Control of a UAV with Inflatable Wings with Wing Warping
AIAA-2006-1697 Development of a Finite Element Model of Warping Inflatable Wings
AIAA-2006-1805 Measurement of In-Plane Motion of Thin-Film Structures Using Videogrammetry
AIAA-2006-1696 A High-Altitude Test of Inflatable Wings for Low-Density Flight Applications
WorldSID Assessment of Far Side Impact Countermeasures