Outer Planet Entry Heating and Thermal ProtectionRaymond Viskanta |
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Page 346
... boundary - layer velocity thickness boundary - layer displacement thickness shear - layer velocity profile similarity parameter , n = oY / x boundary - layer momentum thickness ; also central angle absolute viscosity density shear ...
... boundary - layer velocity thickness boundary - layer displacement thickness shear - layer velocity profile similarity parameter , n = oY / x boundary - layer momentum thickness ; also central angle absolute viscosity density shear ...
Page 351
... boundary - layer profile persists downstream in the outer profile . This initial boundary - layer profile is determined from integral relation- ships embodied in the TOPIC forebody code . 5 The effect of the initial boundary layer has ...
... boundary - layer profile persists downstream in the outer profile . This initial boundary - layer profile is determined from integral relation- ships embodied in the TOPIC forebody code . 5 The effect of the initial boundary layer has ...
Page 389
... boundary layers.2-7 However , these studies did not emphasize data for which the boundary layer was orders of magnitude thicker than the corrugation height . The first detailed investigation of heat transfer to corrugations deeply ...
... boundary layers.2-7 However , these studies did not emphasize data for which the boundary layer was orders of magnitude thicker than the corrugation height . The first detailed investigation of heat transfer to corrugations deeply ...
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