Interactive-boundary-layer method developed for computations of steady flow, extended under assumption of quasi-steady flow, to computations of evolution of two-dimensional flow about oscillating airfoil under light-dynamic-stall conditions. Represents advance toward ability to compute unsteady flows at even greater angles of attack with solutions of equations normally used for description of boundary-layer flows on airfoils prior to stall. Important in practical studies of flow on blades of helicopter rotors, axial compressors, and turbines.


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    Titel :

    Interactive-Boundary-Layer Computations For Oscillating Airfoil


    Beteiligte:
    Carr, L. W. (Autor:in) / Cebeci, T. (Autor:in) / Jang, Hong-Ming (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1993-02-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :