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On board water recovery for water injection in high efficiency gasoline engines
Apollo IV (AS-501): Convective Heating Predictions of Flight Data
Combustion Generated Heat Addition to a Ducted Supersonic Stream. I. Theory
Stagnation Point Flow with Radiation
A Study of Propellant Behavior at Zero Gravity Final Report
An Analysis of a Charring Ablation Thermal Protection System
Three-dimensional Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow