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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    Title :

    Airfoil Profile in a Nonuniform Flow


    Contributors:
    J. Polasek (author)

    Publication date :

    1978


    Size :

    53 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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