Usefulness of boundary layer control (BLC) at knee of trailing edge flap, over wing nose close to leading edge or at knee of leading edge flap is shown; various methods of providing BLC are outlined, comprising slot blowing, slot suction, area suction, inclined air jets, and specially designed airfoil shapes; aerodynamic aspects of slot blowing over trailing edge flaps and wing nose are examined, and slot and area suction considered; associated practical design features required for good performance are discussed and some flight handling implications mentioned. (See also AGARD -- Report 414 Jan 1963 69 p)


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    Title :

    Aerodynamic aspects of boundary layer control for high lift at low speeds


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1963


    Size :

    23 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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