Predictive Control Design for an Unmanned Aerial Vehicle
Evaluation of Heat Pipes in the Temperature Range of 450 to 700 K
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
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
Thermo-Physical Properties of Intermediate Temperature Heat Pipe Fluids
Water Heat Pipe Radiator Trade Study for the 300-550 K Temperature Range
AIAA-2004-5084 F/A-22 High Angle of Attack Buffet - Test Adequacy Analysis
AIAA-2004-1678 Low Speed Wind Tunnel Buffet Testing on the F/A-22
Passive Thermal Management for Avionics in High Temperature Environments
Standardization of Environmental Requirements for Warship Control Equipment
Propulsion Educational and Research Programs at Purdue University AIAA Paper
Aerodynamic Design Optimization on Unstructured Grids with a Continuous Adjoint Formulation
AIAA-2001-0596 Recent Improvements in Aerodynamic Design Optimization On Unstructured Meshes