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    Title :

    AIAA-2004-5193 Subsonic Aerodynamic Fin Folding Moments for the Tactical Tomahawk Missile Configuration


    Contributors:
    McGrath, B. (author)

    Conference:

    22nd, AIAA applied aerodynamics conference ; 2004 ; Providence, RI



    Publication date :

    2004-01-01


    Size :

    9 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English