Results of investigation made in NACA 7 by 10-ft wind tunnel; static rolling and yawing moments were determined for all devices tested, and static hinge moments and time response were determined for few devices of each type.


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    Title :

    Wind-tunnel investigation of spoiler, deflector, and slot lateral-control devices on wings with full-span split and slotted flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1941


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English