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    Title :

    Wind-tunnel investigation of an NACA 23021 airfoil with two sizes of balanced split flaps


    Contributors:

    Publication date :

    1941


    Size :

    13 S., [19] Bl


    Remarks:

    graph. Darst
    Originally issued February 1941 as Advance confidential report
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik



    Wind-tunnel investigation of NACA 23021 airfoil with two sizes of balanced split flaps

    Swanson, R.S. / Schuldenfrei, M.J. | Engineering Index Backfile | 1941



    Wind-tunnel investigation of N.A.C.A. 23021 airfoil with various arrangements of slotted flaps

    Wenzinger, C.J. / Harris, T.A. | Engineering Index Backfile | 1939


    Pressure distribution over NACA 23021 airfoil with slotted and split flap

    Harris, T.A. / Lowry, J.G. | Engineering Index Backfile | 1941


    Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap

    Harris, T.A. / Purser, P.E. | Engineering Index Backfile | 1940