Development of a Novel Low Stored Volume High-Altitude Wing Design
Development and Flight Testing of a UAV with Inflatable-Rigidizable Wings
Design Limitations of Deployable Wings for Small Low Altitude UAVS
Design Limitations of Deployable Wings for Small Low Altitude UAVs
Designing Collaborative Automated Planners for Agile Adaptation to Dynamic Change
Design and Flight Testing of Inflatable Wings with Wing Warping
Design and Development of a Crash Referencing and Analysis System
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
BIG BLUE II: Mars Aircraft Prototype with Inflatable-Rigidizable Wings
BIG BLUE: High-Altitude UAV Demonstrator of Mars Airplane Technology
Autonomous Structural Health Monitoring System: A Demonstration
Automated and Enhanced Assessment of Unilateral Visual Neglect
Auditory Warnings in the Cockpit: An Evaluation of Potential Sound Types
ASSET-2: Real-Time Motion Segmentation and Shape Tracking
A Scene Segmenter; Visual Tracking of Moving Vehicles
A Reusable Space Vehicle Design Study Exploring Sharp Leading Edges
A Research Agenda for the North American Travel Industry
A Proposed Method to Standardize Shock Response Spectrum (SRS) Analysis
A Pressurized Deployment Model for Inflatable Space Structures
A Preliminary Evaluation of Child Restraints and Anchorage Systems for an Australian Car
A Preliminary Design Study of a Joint Primary Aircraft Trainer (JPAT)
A New Model to Improve Aggregate Air Traffic Demand Predictions AIAA Paper
An Evaluation of Mixed-Mode Energy-Release Rates in the Cracked Sandwich Beam Specimen
Altitude Comparison Technique Using the MC-130H APN-232 RADAR Altimeter
A Light-Weight, Improved Performance Truck for the Trinity HPIT Car
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-2004-6570 Flying on Air: UAV Flight Testing with Inflatable Wing Technology
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
Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing AIAA Paper
ADVANCED MULTIDISCIPLINARY OPTIMIZATION TECHNIQUES FOR EFFICIENT SUBSONIC AIRCRAFT DESIGN
A Coupled Aero-Structural Optimization Method for Complete Aircraft Configurations
2012-01-1092 Electrically Heated Catalysts for Cold-Start Emissions in Diesel Aftertreatment