Shock layer properties, radiative and convective heat transfer about two hypersonic blunt bodies at zero angle of attack in assumed Martian atmosphere
Theoretical evaluation of the simulation of radiative heating of planetary entry vehicles.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, THERMOPHYSICS CONFERENCE ; 1969 ; SAN FRANCISCO, CALIF.
01.06.1969
Aufsatz (Konferenz)
Keine Angabe
Englisch
Simulation of planetary entry radiative heating with a C1O2 gasdynamic laser
Tema Archiv | 1975
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