Solution for blunt body flow is presented; approximation is based on flow being hypersonic, which implies density ratio across shock wave is small; consideration is restricted to axisymmetric bodies for which solution can be written in analytic form. (14169)


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    Title :

    Series solution for hypersonic flow about blunt bodies


    Additional title:

    NASA CR


    Contributors:
    Chou, Y.S. (author)

    Published in:

    Publication date :

    1969


    Size :

    82 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :





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