A description is given of the computational codes that are to be used in studies of the heating and aerodynamic performance of entry probes for the scientific exploration of the planets Jupiter, Saturn, and Uranus. These codes include a time-asymptotic numerical method which takes into account radiative transport and equilibrium chemistry for the direct solution of the radiative, inviscid flow over an axisymmetric or two-dimensional body. The method considers both supersonic and subsonic flow in the downstream region. Another code represents a laminar, viscous-shock-layer solution.
Outer planet entry probes aerothermal environment - Status of prediction methodology
American Institute of Aeronautics and Astronautics and American Geophysical Union, Conference on the Exploration of the Outer Planets
1975-09-01
Conference paper
No indication
English
Aerothermal environment for Jovian entry probes
AIAA | 1976
|Radiative heating about outer planet entry probes
AIAA | 1975
|Radiative Heating About Outer Planet Entry Probes
AIAA | 1976
|