Base pressure distribution on blunted cones during supersonic wind tunnel tests


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    Title :

    Base pressure distribution of two blunted cones at Mach numbers from 0.3 to 0.8 and 1.81 to 3.51


    Contributors:
    Kerr, W. R. (author) / Kurtz, D. W. (author)

    Publication date :

    1968-10-15


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :