2008-01-0777 Experimental Validation of a Coupled Fluid-Multibody Dynamics Model for Tanker Trucks
2012-01-1092 Electrically Heated Catalysts for Cold-Start Emissions in Diesel Aftertreatment
ADVANCED MULTIDISCIPLINARY OPTIMIZATION TECHNIQUES FOR EFFICIENT SUBSONIC AIRCRAFT DESIGN
Aeroelastic Behavior of Inflatable Wings: Wind Tunnel and Flight Testing AIAA Paper
AIAA-2001-1264 Experimental Results Regarding the Inflation of Unfolding Cylindrical Tubes
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
AIAA-2006-1696 A High-Altitude Test of Inflatable Wings for Low-Density Flight Applications
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
Altitude Comparison Technique Using the MC-130H APN-232 RADAR Altimeter
A New Model to Improve Aggregate Air Traffic Demand Predictions AIAA Paper
A Preliminary Evaluation of Child Restraints and Anchorage Systems for an Australian Car
A pressurized deployment model for inflatable space structures
A Pressurized Deployment Model for Inflatable Space Structures
A Proposed Method to Standardize Shock Response Spectrum (SRS) Analysis
A Research Agenda for the North American Travel Industry
A Reusable Space Vehicle Design Study Exploring Sharp Leading Edges
ASSET-2: Real-Time Motion Segmentation and Shape Tracking
Autonomous Structural Health Monitoring System: A Demonstration
BIG BLUE II: Mars Aircraft Prototype with Inflatable-Rigidizable Wings
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
Combination Resonance Nonlinear Response in the MIR Structural Dynamics Experiement (MISDE) Data
Comparison of a Zymate System V Controller to a Zymate II Controller
Computational Issues for Two Multiple Constraint Stiffness Matrix Adjustment Methods
Design and Development of a Crash Referencing and Analysis System
Design and Flight Testing of Inflatable Wings with Wing Warping
Designing Collaborative Automated Planners for Agile Adaptation to Dynamic Change
Design Limitations of Deployable Wings for Small Low Altitude UAVS
Design Limitations of Deployable Wings for Small Low Altitude UAVs
Development and Flight Testing of a UAV with Inflatable-Rigidizable Wings
Development of a Novel Low Stored Volume High-Altitude Wing Design
Developments in Large-Scale, Audio-Frequency, Data Acquisition/Analysis System Technology
Diagnostic Assistant Based on Graphical Probabilistic Models
Diagnostic Assistant Based on Graphical Probabilistic Models
Director 4.0 For The Macintosh: First Half Of A Major Release
Effect of Boundary Conditions on Geometric Control for an Inflatable Pathfinder System