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Viscous-shock-layer solutions for turbulent flow of radiating gas mixtures in chemical equilibriumThe viscous-shock-layer equations for hypersonic laminar and turbulent flows of radiating or nonradiating gas mixtures in chemical equilibrium are presented for two-dimensional and axially-symmetric flow fields. Solutions were obtained using an implicit finite-difference scheme and results are presented for hypersonic flow over spherically-blunted cone configurations at freestream conditions representative of entry into the atmosphere of Venus. These data are compared with solutions obtained using other methods of analysis.
Document ID
19750020301
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, E. C. (Old Dominion Univ. Norfolk, VA, United States)
Moss, J. N. (NASA Langley Res. Center)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-143204
TR-75-T9
Accession Number
75N28373
Funding Number(s)
CONTRACT_GRANT: NSG-1065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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