Report presents results of computations and measurements of compressible flow about an airfoil, angle of attack of which oscillates about static-stall angle. Study focuses on effects of compressibility on dynamic stall. Of particular interest are conditions determining onset of separation of flow, which leads to premature dynamic stall and consequent significant reduction of lift.


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    Title :

    Effects Of Compressibility On Dynamic Stall


    Contributors:
    Carr, L. W. (author) / Fung, K.-Y. (author)

    Published in:

    Publication date :

    1992-05-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


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