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Influence of nonequilibrium radiation on heating of an ablating Jovian entry probeThe influence of non-local thermodynamic equilibrium (NLTE) radiative transfer on the entire shock-layer flow phenomena around a Jovian entry body is investigated. The flow in the shock layer is assumed to be viscous, axisymmetric, laminar, and in chemical equilibrium. The entry body considered is a 35-deg hyperboloid and the results have been obtained for the peak heating entry conditions. The results indicate that the radiative heating of the entry body is significantly higher under NLTE conditions.
Document ID
19800039778
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tiwari, S. N.
(Old Dominion Univ. Norfolk, VA, United States)
Subramanian, S. V.
(Old Dominion University Norfolk, Va., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 80-0356
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 14, 1980
End Date: January 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A23948
Funding Number(s)
CONTRACT_GRANT: NSG-1500
Distribution Limits
Public
Copyright
Other

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