THE THOR PROJECT IMPROVED THUNDERSTORM FORECASTS FOR AVIATION AND THE GENERAL PUBLIC
Testing of Compact Inflatable Wings for Small Autonomous Aircraft
Stowed Unmanned Air Vehicle Engineering (SUAVE): Deployable Wing Design and Testing
Standardised Interoperability of Earth Observation Data Catalogues
Staged Microgravity Deployment of a Pressurizing Scale Model Spacecraft
SPICE modeling of ferroelectric liquid crystal on silicon microdisplays [5181-21]
Simulation of Deployment Dynamics of an Inflatable Solar Array
Preliminary Survey of Nonlinear Response Behaviors of a Solar Array Phenomena Model
Preliminary Evaluation of the Effects of Aircraft Seat Cushions on Human Vibration Response
Post-Flight Testing and Analysis of Zero-G Foam Rigidized Struts
Modeling the Dynamics of Large Diameter Doubly Curved Shells made from Thin-Films
Modeling and Characterization of Damage Processes in Metallic Materials
Measurement of Three Dimensional Eye Position using Image Processing: A Geometric Approach
Feedback neural network for pattern recognition [3647-23]
Experimental Results Regarding Two-Dimensional Deployment of Inflatable Beams
Experimental Characterization of Hydrocarbon-Fueled, Axisymmetric, Scramjet Combustor Flowpaths
Development of a Novel Low Stored Volume High-Altitude Wing Design
Computational Issues for Two Multiple Constraint Stiffness Matrix Adjustment Methods
Combination Resonance Nonlinear Response in the MIR Structural Dynamics Experiement (MISDE) Data
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
Autonomous Structural Health Monitoring System: A Demonstration
Automated and Enhanced Assessment of Unilateral Visual Neglect
ASSET-2: Real-Time Motion Segmentation and Shape Tracking
A Pressurized Deployment Model for Inflatable Space Structures
An Evaluation of Mixed-Mode Energy-Release Rates in the Cracked Sandwich Beam Specimen
AIRCRAFT MEASUREMENTS AND SIMULATIONS OF MOUNTAIN WAVES OVER MONT BLANC
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
AIAA-2001-1264 Experimental Results Regarding the Inflation of Unfolding Cylindrical Tubes