Results show that wing equipped with group of spoiler segments located near wing trailing edge, slightly inboard from wing tip, and skewed with reference to wing so as to be perpendicular to free stream air flow will exhibit fairly high values of rolling moment throughout usable lift range.


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    Titel :

    Low-speed wind-tunnel investigation of various plain-spoiler configurations for lateral control on 42° sweptback wing


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Schneiter, L.E. (Autor:in) / Watson, J.M. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    29 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch