Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page 93
... equations to evaluate the nine unknowns p , V , u , P , h , H , CH , and CH The solutions of this set of algebraic equations are obtained by using ... equation , and C , in the species continuity equations INFLUENCE OF PRECURSOR HEATING 93.
... equations to evaluate the nine unknowns p , V , u , P , h , H , CH , and CH The solutions of this set of algebraic equations are obtained by using ... equation , and C , in the species continuity equations INFLUENCE OF PRECURSOR HEATING 93.
Page 132
... equations and boundary conditions for the present problem are essentially the same as given in Ref . 2. There are , however , a few definite changes in the governing equations because of the chemical nonequilibrium condition , and these ...
... equations and boundary conditions for the present problem are essentially the same as given in Ref . 2. There are , however , a few definite changes in the governing equations because of the chemical nonequilibrium condition , and these ...
Page 171
... equations used in the present work are given by Murray and Lewis . 8 Shock Conditions . The shock boundary conditions with slip are the modified Rankine - Hugonoit equations used by Davis.1 The angle between the freestream velocity ...
... equations used in the present work are given by Murray and Lewis . 8 Shock Conditions . The shock boundary conditions with slip are the modified Rankine - Hugonoit equations used by Davis.1 The angle between the freestream velocity ...
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