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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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English