Results of tests of wing sections characterized by small travel of the center of pressure, tested at 20-atmos pressure in variable-density wind tunnel of Nat. Advisory Committee for Aeronautics, giving consistent results and showing that for stable sections a small effective camber, a small effective S-shape and a thickness of 8 to 12 per cent, lead to good aerodynamic properties.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Model tests with a systematic series of 27 wing sections at full Reynolds number


    Weitere Titelangaben:

    U.S. Nat. AdvisoryComm. Aeronautics -- Report


    Beteiligte:
    Munk, M.M. (Autor:in) / Miller, E.W. (Autor:in)


    Erscheinungsdatum :

    1925


    Format / Umfang :

    18 pages


    Anmerkungen:

    27 Figs.


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :






    Investigation of Faceted Wing Sections for Low Reynolds Number Applications

    Gautam, Mridul / Browning, Patrick H. / Huebsch, Wade | SAE Technical Papers | 2013