Spatial approaches to moons from resonance relative to invariant manifolds
Spatial approaches to moons from resonance relative to invariant manifolds
Evaluation of Heat Pipes in the Temperature Range of 450 to 700 K
Predictive Control Design for an Unmanned Aerial Vehicle
Aerodynamic design optimization on unstructured meshes using the Navier-Stokes equations
Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations
Loop Heat Pipe Radiator Trade Study for the 300-550 K Temperature Range
F-22 Aeroelastic Design and Test Validation AIAA Paper 2007-1764 CD-ROM Number 7
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