Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page 122
... convective blowing corrections are necessary . Of the many parameters tried , the convective blowing correction is ... heating ) is certainly within the accuracy of other approximations used in defining the heating environment with- out ...
... convective blowing corrections are necessary . Of the many parameters tried , the convective blowing correction is ... heating ) is certainly within the accuracy of other approximations used in defining the heating environment with- out ...
Page 158
... convective heating rates increase on the windward side and decrease on the leeward side with increasing angle of attack , but the radiative heating rates show a much larger percentage change than the convective heating rates . As an ...
... convective heating rates increase on the windward side and decrease on the leeward side with increasing angle of attack , but the radiative heating rates show a much larger percentage change than the convective heating rates . As an ...
Page 363
... convective heat - transfer rates is shown in Fig . 14. It is interesting to note that the laminar convective heating is always greater than the turbulent convective heating ; thus a conservative design approach has been taken in always ...
... convective heat - transfer rates is shown in Fig . 14. It is interesting to note that the laminar convective heating is always greater than the turbulent convective heating ; thus a conservative design approach has been taken in always ...
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