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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    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Wenzinger, C.J. (Autor:in) / Rogallo, F.M. (Autor:in)


    Erscheinungsdatum :

    1941


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch