Solutions are presented for the stagnation-region shock-layer equations, including radiative transfer with spectral lines and silica ablation during Jovian entry. Results for variations of entry angle, sphere-cone configuration, and atmospheric model are given. The effect of silica ablation on the radiative and convective surface heating is correlated with the ratio of the wall to free-stream mass flux. Correlations are also given for spectral distributions. The effect of newly obtained SiO radiation properties on the surface heating is examined. (Buehn)
Aerothermodynamic environment for Jovian entry with a silica heat shield
Aerothermodynamische Umgebungseinfluesse auf ein Jupiter-Landegeraet mit einem Siliziumoxid-Hitzeschild
AIAA-Papers ; 1-15
1978
15 Seiten, 13 Bilder, 3 Tabellen, 15 Quellen
Aufsatz (Konferenz)
Englisch