The Application of Tolerance Rings to Provide Shock Overlaod Protection in EPAS Systems
Challenges of Modeling Inflatable Wings AIAA Paper 2007-1848 CD-ROM Number 7
An Aircraft Design Competition for High School STEM Improvement (AIAA 2014-0063)
Development of a Novel Low Stored Volume High-Altitude Wing Design
CFD Assessment of Fin Manufacturing Defect to Set Fin Cant Angle and Achieve Nominal Roll Rate
An Aeroelastic Coupling Framework for Time-accurate Analysis and Optimization (AIAA 2018-0100)
Experimental and Numerical Investigation of Airfoil Performance in Cylinder Wake (AIAA 2018-3232)
AIAA-2004-1950 Helicopter Blade Lag Damping Using Embedded Fluid Elastic Inertial Dampers
Material And Geometric Characteristics In Aluminum Components For Crash Applications
AIAA-2004-1503 Development of UV-Curable Inflatable Wings for Low-Density Flight Applications
Higher Order Finite Element Solutions for Thick Plate Buckling