Discrete-Roughness Transition for Hypersonic Flight Vehicles
Finite Volume Numerical Methods for Aeroheating Rate Calculations from Infrared Thermographic Data
SPECIAL SECTION: X-34 - X-34 Experimental Aeroheating at Mach 6 and 10
SPECIAL SECTION: X-33 AEROTHERMODYNAMICS - X-33 Hypersonic Boundary-Layer Transition
Aeroheating Testing and Predictions for Project Orion Crew Exploration Vehicle