Investigation of maximum lift obtainable with slotted airfoils derived from symmetrical airfoil; center of lift travels contrary to usual direction as angle of attack is increased; tests of series of slotted airfoils derived from dissymmetrical airfoil. Translated from Service Technique de L'Aerotechnique Belge -- Bul., nos. 1 and 4, Apr. and July, 1927.


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    Title :

    Results of aerodynamic tests on slotted airfoils in the aerotechnical laboratory (S. T. Ae.) of Rhone St. Genese, Brussels


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memorandums


    Contributors:
    Puvrez, P. (author)


    Publication date :

    1928


    Size :

    19 pages


    Remarks:

    6 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :