Solution of the inverse boundary value problem of aerohydrodynamics for a two-element airfoil. (English. Russian original) Zbl 1178.76081
Fluid Dyn. 39, No. 3, 367-375 (2004); translation from Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza 2004, No. 3, 16-24 (2004).
Summary: The basic inverse boundary value problem of aerohydrodynamics for a two-element airfoil is analytically and numerically solved in the complete formulation. The problems of designing biplane airfoils and an airfoil with a trailing-edge flap or leading edge flap (slat) are solved for a given distribution over the unknown contours of the velocity or the pressure as a function of the contour arc abscissa of the airfoils which depends on a finite number of the parameters.
MSC:
| 76B10 | Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing |
| 76M40 | Complex variables methods applied to problems in fluid mechanics |
