F-22 Aeroelastic Design and Test Validation AIAA Paper 2007-1764 CD-ROM Number 7
Safety Enhancements Available by Converting MSG-2 Aircraft Maintenance Programs to MSG-3
An MDO approach to Control-Configured-Vehicle design
An MDO Approach to Control-Configured-Vehicle Design
Sensitivity Derivatives for Plasma Discharge Simulations
Sensitivity Derivatives for Plasma Discharge Simulations
A Dynamical Systems Analysis of Resonant Flybys: Ballistic Case
A Dynamical Systems Analysis of Resonant Flybys: Ballistic Case
Fuel Injection Strategies to Increase Full-Load Torque Output of a Direct-Injection SI Engine
Multiscale Large Eddy Simulation of Turbulence Using High-Order Finite Element Methods
Multiscale Large Eddy Simulation of Turbulence Using High-Order Finite Element Methods
Dynamical Systems Analysis of Planetary Flybys and Approach: Planar Europa Orbiter
A General and Extensible Unstructured Mesh Adjoint Method
A General and Extensible Unstructured Mesh Adjoint Method