Geodesic
About the Problem of Two-Element Airfoil Optimization
Učënye zapiski Kazanskogo universiteta. Seriâ Fiziko-matematičeskie nauki, Kazanskii Gosudarstvennyi Universitet. Uchenye Zapiski. Seriya Fiziko-Matematichaskie Nauki, Tome 150 (2008) no. 1, pp. 19-2 Cet article a éte moissonné depuis la source Math-Net.Ru

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A numerical solution is presented for the problem of finding an optimal two-element wing airfoil shape with maximum lift coefficient flowed by a subsonic viscous non-separation stream. The solution method is based on the theory of inverse boundary-value problem of aerohydrodynamics for analytical functions. The effects of viscosity and compressibility within the framework of boundary layer theory and the Chaplygin's gas model are taken into account.
Keywords: optimization, boundary layer, Chaplygin's gas, inverse boundary-value problem of aerohydrodynamics
Mots-clés : two-element airfoil. 
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P. A. Volkov; N. B. Il'inskii. About the Problem of Two-Element Airfoil Optimization. Učënye zapiski Kazanskogo universiteta. Seriâ Fiziko-matematičeskie nauki, Kazanskii Gosudarstvennyi Universitet. Uchenye Zapiski. Seriya Fiziko-Matematichaskie Nauki, Tome 150 (2008) no. 1, pp. 19-2. http://geodesic.mathdoc.fr/item/UZKU_2008_150_1_a1/

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