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Evaluation of one-dimensional approximations for radiative transport in blunt body shock layersOne-dimensional approximations for the nongray radiative flux and flux divergence in radiating shock layers about a blunt entry body are compared with an exact three-dimensional treatment. A coupled radiative-gasdynamic analysis of the shock layer flow about the entire body provided the thermodynamic field used in these comparisons. In terms of calculating the total energy lost by the shock layer, the one-dimensional approximations to the radiative flux divergence are accurate to within a few percent. In terms of calculating the surface flux, the one-dimensional approximations introduce the largest errors of approximately 15 percent near the stagnation point. The source of these errors is the slab-like geometric representation of the shock layer inherent in all one-dimensional models. Finally, for both the radiative flux and its divergence, the tangent slab approximation provides more accurate results than differential approximation methods.
Document ID
19720011665
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilson, K. H.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 6, 2013
Publication Date
March 1, 1972
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-1990
Accession Number
72N19315
Funding Number(s)
CONTRACT_GRANT: NAS2-5749
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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