Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page 52
... obtained with a viscous shock - layer ( VSL ) analysis for the large 45 - deg spherically blunted cone ( RN = 0.381 m ) are compared with corresponding solutions obtained with the present method and a detailed radiating inviscid ...
... obtained with a viscous shock - layer ( VSL ) analysis for the large 45 - deg spherically blunted cone ( RN = 0.381 m ) are compared with corresponding solutions obtained with the present method and a detailed radiating inviscid ...
Page 92
... obtained by using the semiempirical formulas of Wilke , 26 For hydrogen - helium species , relations for viscosity and thermal conductivity are given in Refs . 27 and 28 , and the specific relations used in this study are given in Ref ...
... obtained by using the semiempirical formulas of Wilke , 26 For hydrogen - helium species , relations for viscosity and thermal conductivity are given in Refs . 27 and 28 , and the specific relations used in this study are given in Ref ...
Page 261
... obtained using the " old " line - width model used by Green and Nicolet3 in the spectral range of interest . The ordinate in the figure is the absorbed flux , i.e. , the portion of the radiation incident on the wall which is absorbed by ...
... obtained using the " old " line - width model used by Green and Nicolet3 in the spectral range of interest . The ordinate in the figure is the absorbed flux , i.e. , the portion of the radiation incident on the wall which is absorbed by ...
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/m² 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