Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page 67
... species are mon- atomic carbon and monatomic hydrogen , and the temperature is 7775 K. The mole fractions of the various species at this inner mixing boundary are shown in Table 1. Mixing of the ablative species and the Jovian ...
... species are mon- atomic carbon and monatomic hydrogen , and the temperature is 7775 K. The mole fractions of the various species at this inner mixing boundary are shown in Table 1. Mixing of the ablative species and the Jovian ...
Page 111
... species . The species considered in this study are H , H2 , H , He , Si , Si * , 0 , 0 , 0 , and Si0 . For the equilibrium chemistry calcu- lation , seven species describe the Jovian atmospheric gas mixture : H , H2 , e ̄ , H † , H ...
... species . The species considered in this study are H , H2 , H , He , Si , Si * , 0 , 0 , 0 , and Si0 . For the equilibrium chemistry calcu- lation , seven species describe the Jovian atmospheric gas mixture : H , H2 , e ̄ , H † , H ...
Page 219
... species mole fractions predicted using JANNAF data when compared with the Dolton data predictions differ by a factor of at least 2 for all species in some range of grad , and the difference may be as much as a factor of 30. Results were ...
... species mole fractions predicted using JANNAF data when compared with the Dolton data predictions differ by a factor of at least 2 for all species in some range of grad , and the difference may be as much as a factor of 30. Results were ...
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