Steady and unsteady stall are studied on a rectangular wing in normal flow. The wing is allowed to oscillate in pitch around the fore quarter chord. Experiments performed at the S 2 wind-tunnel in Chalais-Meudon with a rectangular wing and a wind velocity of 95 m/s are in good agreement with the results obtained from the theory developed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Unsteady Three-Dimensional Stall on a Rectangular Wing


    Beteiligte:
    J. J. Costes (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch