Mach number and pressure measurements on afterbody of blunt-nose model in free flight at hypersonic speeds


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    Title :

    Measurements of the Mach number and pressure on the afterbody of a blunt-nosed model in free flight at Mach numbers from 6.5 to 14


    Contributors:

    Publication date :

    1960-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English