The analysis of the influence of the turbulence model selection on the parameters of interaction of a supersonic jet with an obstacle

Due to the intense loading of the elements of launch structures when exposed to rocket engine jets, it is obvious that it is necessary to determine the gas-dynamic, thermal and other loads that occur during the launch of the launch vehicle. Numerical modeling using application programs is one of t...

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Bibliographic Details
Main Authors: R. A. Peshkov, A. S. Shmetkova, O. V. Ispravnikova, Ju. L. Suskina
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education 2024-10-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
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Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2024/%D0%A2.8,%20%E2%84%963%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/90-97%20%D0%9F%D0%B5%D1%88%D0%BA%D0%BE%D0%B2%20%D0%A0.%20%D0%90.,%20%D0%A8%D0%BC%D0%B5%D1%82%D0%BA%D0%BE%D0%B2%D0%B0%20%D0%90.%20%D0%A1.,%20%D0%98%D1%81%D0%BF%D1%80%D0%B0%D0%B2%D0%BD%D0%B8%D0%BA%D0%BE%D0%B2%D0%B0%20%D0%9E.%20%D0%92.,%20%D0%A1%D1%8E%D1%81%D1%8C%D0%BA%D0%B8%D0%BD%D0%B0%20%D0%AE.%20%D0%9B..pdf
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