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

Voir la notice du chapitre de livre provenant de la source Math-Net.Ru

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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     author = {P. A. Volkov and N. B. Il'inskii},
     title = {About the {Problem} of {Two-Element} {Airfoil} {Optimization}},
     journal = {U\v{c}\"enye zapiski Kazanskogo universiteta. Seri\^a Fiziko-matemati\v{c}eskie nauki},
     pages = {19--2},
     publisher = {mathdoc},
     volume = {150},
     number = {1},
     year = {2008},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/UZKU_2008_150_1_a1/}
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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/