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    Title :

    Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.5 degree delta-wing and an unswept horizontal tail


    Contributors:

    Publication date :

    1958-03-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English