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    Title :

    Lateral-control investigation of flap-type controls on a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic bump method


    Contributors:

    Publication date :

    1950-03-02


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English