Tests with three different sized split trailing-edged flaps, in N.A.C.A. 7 by 10-ft wind tunnel; split flaps when deflected about their original axis locations gave slightly higher maximum lift coefficients than conventional trailing-edge flaps, and lift coefficients were increased still further by moving axes toward rear.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic characteristics of model wing having split flap deflected downward and moved to rear


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Beteiligte:
    Weick, F.E. (Autor:in) / Harris, T.A. (Autor:in)


    Erscheinungsdatum :

    1932


    Format / Umfang :

    7 pages


    Anmerkungen:

    11 Supp plates


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :