Pressure tunnel investigation of supersonic store interference in vicinity of 22 deg swept wing fuselage configuration at mach numbers 1.61 and 2.01


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    Title :

    An investigation of supersonic store interference in the vicinity of a 22 deg swept wing fuselage configuration at Mach numbers of 1.61 and 2.01


    Contributors:

    Publication date :

    1958-02-24


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English