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