Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page vii
... Thermophysics is founded on the well - established disciplines of heat and mass transfer , fluid mechanics , thermodynamics and thermophysical properties , solid - state and optical physics , and cryogenics . Its rapid development is ...
... Thermophysics is founded on the well - established disciplines of heat and mass transfer , fluid mechanics , thermodynamics and thermophysical properties , solid - state and optical physics , and cryogenics . Its rapid development is ...
Page x
... thermophysics sessions at the 16th AIAA Aerospace Sciences Meeting . As General Chairman of the 2nd AIAA / ASME Thermophysics and Heat Transfer Conference , I was supported by Dr. John R. Howell as Technical Program Chairman . Dr. Allie ...
... thermophysics sessions at the 16th AIAA Aerospace Sciences Meeting . As General Chairman of the 2nd AIAA / ASME Thermophysics and Heat Transfer Conference , I was supported by Dr. John R. Howell as Technical Program Chairman . Dr. Allie ...
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Raymond Viskanta. 17. Methods in Astrodynamics and Celestial Mechanics . 1966 18. Thermophysics and Temperature Control of Spacecraft and Entry Vehicles . 1966 19. Communications Satellite Systems Technology . 1966 20. Thermophysics of ...
Raymond Viskanta. 17. Methods in Astrodynamics and Celestial Mechanics . 1966 18. Thermophysics and Temperature Control of Spacecraft and Entry Vehicles . 1966 19. Communications Satellite Systems Technology . 1966 20. Thermophysics of ...
Contents
Effects of Atmospheric Structure on Radiative Heating | 3 |
Radiative Flux Penetration through a Blown Shock Layer | 22 |
Approximate Inviscid Radiating Flowfield Analysis | 42 |
Copyright | |
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Common terms and phrases
ablation absorption coefficient AIAA AIAA Journal AIAA Paper altitudes analysis angle of attack base blockage body surface boundary layer bow shock calculations carbon phenolic chemical chemical equilibrium computed configuration correlation distribution energy enthalpy entry conditions equilibrium experimental flow flowfield freestream graphite H₂ heat shield Heat Transfer heat-transfer hydrogen hyperboloid inertial entry angle intensity inviscid Jupiter Jupiter entry km/sec laminar laser mass loss mass transfer material mixture model atmospheres MW/mē NASA nominal nondimensional nonequilibrium number density obtained Outer Planet Entry parameters PRECURSOR EFFECT precursor heating precursor region predicted present pressure radiation radiative and convective radiative flux radiative heat flux radiative heating rates recession Reynolds number shock-layer shown in Fig silica solution species spectral spectral flux sphere-cone stagnation point stagnation-point temperature thermal thermochemical thermodynamic tion trajectory turbulent uncertainty variation velocity viscous shock-layer VSL3D wall