Method for evaluating flow field around blunt nosed body of revolution, from stagnation pressure measurements and bow shock shape; results obtained by applying method to hemisphere cylinder body at 7.3 Mach are given and compared with results given by approximate theory.


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    Title :

    Flow field about hemisphere-cylinder body at Mach number of 7.3


    Additional title:

    Sweden. Flygtekniska Forsoksanstalten -- Meddelande (Aeronautical Research Inst Report)


    Contributors:
    Wilby, P.G. (author)


    Publication date :

    1962


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :