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Radiative and convective heating during Venus entry.Determination of the stagnation region heating of probes entering the Venusian atmosphere. Both convective and radiative heat-transfer rates are predicted, and account is taken of the important effects of radiative transport in the vehicle shock layer. A nongray radiative transport model is utilized which parallels a four-band treatment previously developed for air (Page et al., 1969), but includes two additional bands to account for the important CO(4+) molecular band system. Some comparisons are made between results for Venus entry and results for earth entry obtained using a viscous earth entry program.
Document ID
19730025955
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Page, W. A.
Woodward, H. T.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1972
Publication Information
Publication: AIAA Journal
Volume: 10
Subject Category
Aerodynamics
Accession Number
73A10757
Distribution Limits
Public
Copyright
Other

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