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    Title :

    Contributions of Wing, Tail, and Fuselage to the Aerodynamic Characteristics of a Semispan Model of a Supersonic Airplane Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method


    Contributors:

    Publication date :

    1951-07-11


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English