Some recent research on airfoil dynamic stall tentatively defines the boundary-layer flow processes during dynamic stall and suggests an approach to airfoil design for stall delay. The effect of changes of airfoil leading-edge radius and camber on increments in maximum lift coefficients is estimated, using a simple criterion for leading-edge stall. (Author)


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    Title :

    Some Recent Research on Airfoil Dynamic Stall with Application to Airfoil Design


    Contributors:
    N. D. Ham (author)

    Publication date :

    1971


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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