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Mathematical model of the vortex wake in two-dimensional air mission formulation

О.V. Solovyov, S.M. Eryomenko, P.V. Prusak, V.V. Sokolova
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The approach to vortex wake mathematical modeling behind the arbitrary shape bodies in a non-linear non-stationary air mission formulation for the case of two-dimensional flow is given. Mathematical correctness of presented calculation method is shown.
Keywords: vortex wake, mathematical model, discrete vortex method, two-dimensional air mission formulation