Wind tunnel tests at Mach 1.60, 2.36, and 2.96 to determine flow field properties near arrow wing body model for locating potential engine air inlets


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    Title :

    Flow field properties near an arrow wing-body model at Mach numbers of 1.60, 2.36, and 2.96


    Contributors:

    Publication date :

    1968-10-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :