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.


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    Title :

    Unsteady Three-Dimensional Stall on a Rectangular Wing


    Contributors:

    Publication date :

    1988


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English