Determination of the stagnation region heating of probes entering the Venusian atmosphere. Both convective and radiative heat-transfer rates are predicted, and account is taken of the important effects of radiative transport in the vehicle shock layer. A nongray radiative transport model is utilized which parallels a four-band treatment previously developed for air (Page et al., 1969), but includes two additional bands to account for the important CO(4+) molecular band system. Some comparisons are made between results for Venus entry and results for earth entry obtained using a viscous earth entry program.
Radiative and convective heating during Venus entry.
AIAA Journal ; 10
1972-10-01
Sonstige
Keine Angabe
Englisch
Radiative and convective heating during Venus entry.
AIAA | 1972
|Radiative and convective heating during atmospheric entry
TIBKAT | 1968
|