Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page 7
... calculations were made for gas compositions which are not consistent with the particular atmospheric structures . This procedure was done in order to assess separately the effects of atmospheric structure and gas composition ...
... calculations were made for gas compositions which are not consistent with the particular atmospheric structures . This procedure was done in order to assess separately the effects of atmospheric structure and gas composition ...
Page 277
... calculations . Presently work is being carried out to include the effects of aluminum particles on both the flowfield and ablation calculations . This will include the addition of two - phase flow to the time - dependent hydrodynamic ...
... calculations . Presently work is being carried out to include the effects of aluminum particles on both the flowfield and ablation calculations . This will include the addition of two - phase flow to the time - dependent hydrodynamic ...
Page 303
... calculations for the flight envelope and trajectory . The table presents the un- certainty intervals for both QR and Qcy at the stagnation point and the midcone . The associated weighting functions are considered in the discussion on ...
... calculations for the flight envelope and trajectory . The table presents the un- certainty intervals for both QR and Qcy at the stagnation point and the midcone . The associated weighting functions are considered in the discussion on ...
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