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