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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    Titel :

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


    Beteiligte:
    N. D. Ham (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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