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  • 1
    Publication Date: 2019-06-27
    Description: The 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.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-CR-143204 , TR-75-T9
    Format: application/pdf
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