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Estimates of nonequilibrium radiation for Venus entryThe present investigation is an analysis of the radiation from the chemical nonequilibrium region in the shock layer about a vehicle during Venus entry. The radiation and the flow were assumed to be uncoupled. An inviscid, nonequilibrium flowfield was calculated and an effective electronic temperature was determined for the predominant radiating species. Species concentrations and electronic temperature were then input into a radiation transport code to calculate heating rates. The present results confirm earlier investigations which indicate that the radiation should be calculated using electronic temperatures for the radiating species. These temperatures are not related in a simple way to the local translational temperature. For the described mission, the nonequilibrium radiative heating rate is approximately twice the corresponding equilibrium value at peak heating.
Document ID
19750049404
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Grose, W. L.
Nealy, J. E.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
April 1, 1975
Publication Information
Publication: AIAA Journal
Volume: 13
Subject Category
Aerodynamics
Accession Number
75A33476
Distribution Limits
Public
Copyright
Other

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