Annotation
A new numerical algorithm for computation of gas supersonic flows based on the system of quasi-gas dynamic equations has been described and tested. A stationary problem about on axially symmetric flow around a cylinder and a nonstationary problem on a plane flow in a channel with a ledge has been considered. The results of computations demonstrate high precision and efficiency of the algorithm.
© 2016 Publisher M.V.Lomonosov Moscow State University
Authors
T.G. Elizarova, M.E. Sokolova
Department of Mathematics, Faculty of Physics, Moscow State University, Leninskie Gory, Moscow, 119992, Russia
Department of Mathematics, Faculty of Physics, Moscow State University, Leninskie Gory, Moscow, 119992, Russia
Science News of the Faculty of Physics, Lomonosov Moscow State University
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