Abstract
The problem of designing a symmetrical airfoil with a piecewise-constant velocity distribution on its contour is considered. A range of governing parameters corresponding to physically realizable airfoils is determined. The optimal properties of the airfoils constructed are studied.
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Leont'ev, V.G., Potashev, A.V. Model High-Lift Airfoils with Two Constant-Velocity Segments on Their Contours. Fluid Dynamics 36, 866–870 (2001). https://doi.org/10.1023/A:1017950223454
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DOI: https://doi.org/10.1023/A:1017950223454