Tests conducted in NACA 7 by 10 ft tunnel to ascertain aerodynamic characteristics, which involved determination of best slot gap opening, effects of slot width, and effect of trailing edge flap; results of tests.


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    Title :

    Wind-tunnel tests of Clark Y wing with "maxwell" leading-edge slots


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1937


    Size :

    6 pages


    Remarks:

    9 Supp sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :