Other
Scientific paper
Sep 1975
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975aiaa.confr....s&link_type=abstract
American Institute of Aeronautics and Astronautics and American Geophysical Union, Conference on the Exploration of the Outer Pl
Other
Aerothermodynamics, Atmospheric Entry, Outer Planets Explorers, Prediction Analysis Techniques, Ablative Nose Cones, Atmospheric Models, Computer Techniques, Convective Heat Transfer, Laminar Heat Transfer, Radiative Heat Transfer, Technology Assessment, Turbulent Heat Transfer
Scientific paper
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.
Falanga R. A.
Moss James N.
Olstad W. B.
Sutton Kenneth
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