Results of wing tests to determine increase in lift obtainable by boundary layer control and to determine power required for blower.


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    Title :

    Boundary-layer-control tests of two wings in Langley propeller-research tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1946


    Size :

    11 pages


    Remarks:

    20 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :