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    Title :

    Free-flight Investigation at Mach Numbers from 0.8 to 1.5 of the Effect of a Fuselage Indentation on the Zero-lift Drag of a 52.5 Degree Sweptback-wing--body Configuration with Symmetrically Mounted Stores on the Fuselage


    Contributors:

    Publication date :

    1958-02-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English