Entry Heating and Thermal Protection: Technical Papers from the AIAA 17th Aerospace Sciences Meeting, January 1979, and the AIAA 14th Thermophysics Conference, June 1979, Subsequently Revised for this VolumeWalter B. Olstad, American Institute of Aeronautics and Astronautics |
Contents
Methods for Predicting OffStagnationPoint Flowfields for Planetary | 26 |
Nonequilibrium Radiative Heating of a Jovian Entry Body | 83 |
Probe at High Altitudes | 104 |
Copyright | |
11 other sections not shown
Common terms and phrases
ablation absorption AIAA AIAA Paper altitudes angle atomic body boundary layer calculations calorimeter carbon phenolic carbon species centerline chemical chemical equilibrium coefficient collisional computed configuration convective convective heating correlation corrugation effects electron energy enthalpy entry conditions Entry Heating equations equilibrium experimental factor flight flow flowfield freestream FRSI frustum Galileo probe graphite heat shield heat transfer heating rates hydrogen hyperboloid hypersonic Jovian entry Jupiter Jupiter entry laminar LRSI Mach number mass measured NASA NLTE nondimensional nonequilibrium number density obtained Orbiter panel parameter peak heating predicted present pressure gradient radiation radiative flux radiative heat flux Radiative Transfer radius RASLE ratio Reynolds number shock layer shock tube shown in Fig solutions spectral spectral flux stagnation point stagnation-point surface temperature test article Thermal Protection thickness tion total enthalpy trajectory transition uncertainties vapor velocity viscous wall wave