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