Predictive Control Design for an Unmanned Aerial Vehicle
Evaluation of Heat Pipes in the Temperature Range of 450 to 700 K
Aerodynamic design optimization on unstructured meshes using the Navier-Stokes equations
Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations
F-22 Aeroelastic Design and Test Validation AIAA Paper 2007-1764 CD-ROM Number 7
Loop Heat Pipe Radiator Trade Study for the 300-550 K Temperature Range
An MDO approach to Control-Configured-Vehicle design
An MDO Approach to Control-Configured-Vehicle Design
Safety Enhancements Available by Converting MSG-2 Aircraft Maintenance Programs to MSG-3
Fuel Injection Strategies to Increase Full-Load Torque Output of a Direct-Injection SI Engine
Sensitivity Derivatives for Plasma Discharge Simulations
Sensitivity Derivatives for Plasma Discharge Simulations
Multiscale Large Eddy Simulation of Turbulence Using High-Order Finite Element Methods
Multiscale Large Eddy Simulation of Turbulence Using High-Order Finite Element Methods
A General and Extensible Unstructured Mesh Adjoint Method
A General and Extensible Unstructured Mesh Adjoint Method
Spark Anemometry of Bulk Gas Velocity at the Plug Gap of a Firing Engine
Finite-Element Solutions for Turbulent Flow over the NACA 0012 Airfoil (Invited) (AIAA 2015-1531)
Shore-Based Reference Facility (SRF) Requirements for Platform Management Systems