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:
    Polasek, J. (Autor:in)

    Erscheinungsdatum :

    01.03.1978


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Cambered Joukowsky airfoil in a nonuniform weak shear flow

    GUPTA, A. K. / SHARMA, S. C. | AIAA | 1974



    Thin Airfoil in Nonuniform Parallel Streams

    L. Ting / C. H. Liu | NTIS | 1969