Abstract
The calculation features of the turbulent flows described by the Reynolds equations and the two-equation model of turbulence are examined for an explicit high-order accurate Godunov method. Under these features, a new version of a high order of Godunov’s method is developed for calculating the compressible turbulent flows. To illustrate the capability of the new method, some results of the calculation are shown for a supersonic turbulent jet with a complex shock-wave structure and for a separate flow in a plane nozzle.
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Original Russian Text © G.S. Glushko, I.E. Ivanov, I.A. Kryukov, 2009, published in Matematicheskoe Modelirovanie, 2009, Vol. 21, No. 12, pp. 103–121.
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Glushko, G.S., Ivanov, I.E. & Kryukov, I.A. Computational method for turbulent supersonic flows. Math Models Comput Simul 2, 407–422 (2010). https://doi.org/10.1134/S2070048210040010
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DOI: https://doi.org/10.1134/S2070048210040010