NASA NTRS · 19780013105
Airfoil profile in a nonuniform flow
Abstract
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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Polasek, J.. 1978-03-01. Airfoil profile in a nonuniform flow. https://ntrs.nasa.gov/citations/19780013105
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