A theory of airfoil section past two dimensional nonuniform flow is developed. The theory is based on representation of airfoil section by vortex and source distributions and it can be used for calculation of aircraft wings in homogeneous and inhomogeneous flow, as well as for calculation of straight and radial blade and vane-cascades.


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    Titel :

    Airfoil Profile in a Nonuniform Flow


    Beteiligte:
    J. Polasek (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    53 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Airfoil profile in a nonuniform flow

    Polasek, J. | NTRS | 1978



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