Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page 7
... Table 1 ) for which the inertial azimuth angle is 72.5 deg and the latitude at entry is -6.5 deg . Also , trajectory calculations for equatorial entry at a -9 deg iner- tial entry angle were made . The off - equatorial entry is ...
... Table 1 ) for which the inertial azimuth angle is 72.5 deg and the latitude at entry is -6.5 deg . Also , trajectory calculations for equatorial entry at a -9 deg iner- tial entry angle were made . The off - equatorial entry is ...
Page 76
... Table 8 for the pure Jovian atmos- phere are from Biolsi.10 The trends in Tables 5 and 11 of that paper suggest that there is a monotonic decrease in the thermal conductivity from the shock front to the outer mixing boundary . Of ...
... Table 8 for the pure Jovian atmos- phere are from Biolsi.10 The trends in Tables 5 and 11 of that paper suggest that there is a monotonic decrease in the thermal conductivity from the shock front to the outer mixing boundary . Of ...
Page 315
... Tables 2 and 3 were modified by using the nominal conditions , so that the heat - shield recession uncertainty was calculated in units of centimeters . The tables represent the evaluation of the un- certainty as given by Eq . ( 5 ) . Table ...
... Tables 2 and 3 were modified by using the nominal conditions , so that the heat - shield recession uncertainty was calculated in units of centimeters . The tables represent the evaluation of the un- certainty as given by Eq . ( 5 ) . Table ...
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 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 Progress in Astronautics 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