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Authors: P. V. Bulata and K. N. Volkova,b
Affiliations: aSt. Petersburg National Research University of Information Technologies, Mechanics, and Optics, 49 Kronverkskii Ave., St. Petersburg, 197101, Russia; bSchool of Mechanics and Automotive Engineering, Faculty of Science, Engineering and Computing, Kingston University, Friars Ave., Roehampton Vale, London, SW15 3DW, UK; email: dsci@mail.ru.
Abstract: A numerical simulation of flow in a channel with a right-angled step has been performed on nonstructured meshes having different resolving powers with the use of high-accuracy WENO schemes. The calculated shockwave structure of this flow was compared with analogous structures described in the literature. Accuracy criteria of numerical calculations, associated with the position of shock-wave structures, are discussed. Recommendations on practical use of high-accuracy difference schemes for calculations on nonstructured meshes are given.
Keywords: channel, step, supersonic flow, numerical simulation, WENO scheme.
Russian original pages: Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 88, No. 4, pp. 848–855, July–August, 2015.
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The online version of the original article can be found under doi:10.1007/s10891-015-1263-x.
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Bulat, P.V., Volkov, K.N. Erratum to: Simulation of Supersonic Flow in a Channel with a Step on Nonstructured Meshes with the Use of the Weno Scheme. J Eng Phys Thermophy 88, 1582 (2015). https://doi.org/10.1007/s10891-015-1346-8
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DOI: https://doi.org/10.1007/s10891-015-1346-8