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Solution of the problem of optimum boundary layer control on the porous surface of a turbine blade
Authors:L V Bezgin  A N Ganzhelo
Abstract:Problems of the optimization of coolant injection into a laminar compressible gas boundary layer are considered within the framework of the integral method of boundary layer calculation 1].Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No.6, pp. 17–24, November–December, 1993.
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