Numerical solutions are presented for supersonic perfect gas flow; full inviscid equations are used and conditions at shock wave prescribed; body shapes and surface pressure distributions are obtained.


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    Title :

    Calculation of supersonic flow past bodies supporting shock waves shaped like elliptic cones


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :