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  • 11
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    Turbulent viscous-shock-layer solutions with strong vorticity interaction (1976)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Numerical solutions of the viscous-shock-layer equations governing laminar and turbulent flows of a perfect gas and radiating and nonradiating mixtures of perfect gases in chemical equilibrium are presented for hypersonic flow over spherically blunted cones and hyperboloids. The results are compared with boundary-layer and inviscid flow-field solutions. The agreement with the inviscid flow field data is satisfactory. The agreement with boundary-layer solutions is good except in regions of strong vorticity interaction. In these flow regions, the viscous-shock-layer solutions appear to be more satisfactory than the boundary-layer solutions.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 76-120 , Aerospace Sciences Meeting; Jan 26, 1976 - Jan 28, 1976; Washington, DC
    Format: text
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    NASA TECHNICAL REPORTS
  • 12
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    Viscous-shock-layer solutions with radiation and ablation injection for Jovian entry (1975)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: This paper presents results that describe the flow field and surface response conditions for a planetary probe entering the atmosphere of Jupiter. The results are obtained with a viscous-shock-layer analysis which includes mass injection, radiative transfer, diffusion, and viscous effects. Radiative transfer is calculated with an existing nongray radiation model that accounts for molecular band, atomic line, and continuum transitions. Particular emphasis is given to the effect of mass injection on the stagnation and downstream flow. Results for both specified and coupled mass injection are obtained for a carbon heat shield.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 75-671 , American Institute of Aeronautics and Astronautics, Thermophysics Conference; May 27, 1975 - May 29, 1975; Denver, CO
    Format: text
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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