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Three-dimensional Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow
Stagnation Point Flow with Radiation
Combustion Generated Heat Addition to a Ducted Supersonic Stream. I. Theory
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