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    Title :

    Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane-lateral and Directional Stability


    Contributors:

    Publication date :

    1955-04-28


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English