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    Airfoil profile in a nonuniform flow (1978)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: 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.
    Keywords: AERODYNAMICS
    Type: NASA-TM-75272
    Format: application/pdf
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