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    Title :

    Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination with quarter-chord line swept back 32.6 degrees and NACA 65A006 airfoil section


    Contributors:

    Publication date :

    1953-11-20


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English