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Three-dimensional Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow
Stagnation Point Flow with Radiation
Mixing and Demixing Processes in Multiphase Flows with Application to Propulsion Systems
Heat Transfer at Reduced Gravity
Combustion Generated Heat Addition to a Ducted Supersonic Stream. I. Theory
Boundary Layer Transition Correlations and Aeroheating Predictions for Mars Smart Lander
A Study of Propellant Behavior at Zero Gravity Final Report
Apollo IV (AS-501): Convective Heating Predictions of Flight Data
An Analysis of a Charring Ablation Thermal Protection System