X-33 Aerothermal Environment Simulations and Aerothermodynamic Design
Arcjet Semi-Elliptic Nozzle Simulations and Validation in Support of X-33 TPS Testing
Assessment of Laminar, Convective Aeroheating Prediction Uncertainties for Mars-Entry Vehicles
Temperature Constraints at the Sharp Leading Edge of a Crew Transfer Vehicle
Transition Experiments on Blunt Cones with Distributed Roughness in Hypersonic Flight
Transition Experiments on Slightly Blunted Cones with Distributed Roughness in Hypersonic Flight
Computational Fluid Dynamics for Winged Re-entry Vehicles at Hypersonic Conditions