Uncertainty Analysis of Thermal Protection System Response of a Hypersonic Inflatable Aerodynamic Decelerator
46th AIAA Thermophysics Conference
01.01.2016
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hypersonic Inflatable Aerodynamic Decelerator , Thermal Modeling , Thermal Response , Freestream Conditions , Thermal Protection System , Sensitivity Analysis , NASA Langley Research Center , National Full Scale Aerodynamics Complex , Computational Fluid Dynamics , Convective Heat Transfer Coefficient
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