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<article article-type="research-article" dtd-version="1.3" xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xml:lang="ru"><front><journal-meta><journal-id journal-id-type="publisher-id">kaz29</journal-id><journal-title-group><journal-title xml:lang="ru">Вестник Казахстанско-Британского технического университета</journal-title><trans-title-group xml:lang="en"><trans-title>Herald of the Kazakh-British Technical University</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">1998-6688</issn><issn pub-type="epub">2959-8109</issn><publisher><publisher-name>Казахстанско-Британский Технический Университет</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.55452/1998-6688-2023-20-4-85-96</article-id><article-id custom-type="elpub" pub-id-type="custom">kaz29-877</article-id><article-categories><subj-group subj-group-type="heading"><subject>Research Article</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="ru"><subject>МАТЕМАТИЧЕСКИЕ НАУКИ</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>MATHEMATICAL SCIENCES</subject></subj-group></article-categories><title-group><article-title>Численное моделирование существенно дозвуковых течений сжимаемого газа</article-title><trans-title-group xml:lang="en"><trans-title>Numerical modeling of essentially subsonic flows of compressible gas</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0003-1548-7061</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Манапова</surname><given-names>А. К.</given-names></name><name name-style="western" xml:lang="en"><surname>Мanapova</surname><given-names>A.  </given-names></name></name-alternatives><bio xml:lang="ru"><p>Манапова Айнур Қабдешқызы, Магистр прикладной математики и информатики, сениор-лектор</p><p>ул. Ахметова, 44, 050039, г. Алматы</p></bio><bio xml:lang="en"><p>Manapova Ainur, Master of applied mathematics and computer science, Senior Lecturer</p><p>050039, Almaty</p></bio><email xlink:type="simple">manapova.a.k.math@gmail.com</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0003-4360-3728</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Бекетаева</surname><given-names>А. О.</given-names></name><name name-style="western" xml:lang="en"><surname>Beketaeva</surname><given-names>A.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Бекетаева Асель Орозалиевна, Доктор физико-математических наук, главный научный сотрудник</p><p>ул. Пушкина, 125, 050010, г. Алматы</p></bio><bio xml:lang="en"><p>Beketaeva Assel, Доктор физико-математических наук, Главный научный сотрудник института математики и математического моделирования</p><p>ул. Пушкина, 125, 050010, Almaty</p></bio><email xlink:type="simple">azimaras10@gmail.com</email><xref ref-type="aff" rid="aff-2"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0003-4874-5418</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Макаров</surname><given-names>В. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Makarov</surname><given-names>V. </given-names></name></name-alternatives><bio xml:lang="ru"><p>Макаров Вадим Владимирович, Кандидат технических наук, ведущий научный сотрудник</p><p>ул. Профсоюзная, 65, 117997, г. Москва</p></bio><bio xml:lang="en"><p>Makarov Vadim, Кандидат технических наук, Ведущий научный сотрудник</p><p>ул. Профсоюзная, 65, 117997, Moscow</p></bio><email xlink:type="simple">makfone@mail.ru</email><xref ref-type="aff" rid="aff-3"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru">Академиия гражданской авиации<country>Казахстан</country></aff><aff xml:lang="en">Civil Aviation Academy<country>Kazakhstan</country></aff></aff-alternatives><aff-alternatives id="aff-2"><aff xml:lang="ru">Институт математики и математического моделирования КН МОН РК<country>Казахстан</country></aff><aff xml:lang="en">Institute of mathematics and mathematical modeling CS МES RK<country>Kazakhstan</country></aff></aff-alternatives><aff-alternatives id="aff-3"><aff xml:lang="ru">Институт проблем управления РАН; Национальный исследовательский ядерный университет «МИФИ»<country>Россия</country></aff><aff xml:lang="en">Institute of control sciences RAS; National research nuclear university «MEPhI»<country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2023</year></pub-date><pub-date pub-type="epub"><day>12</day><month>12</month><year>2023</year></pub-date><volume>20</volume><issue>4</issue><fpage>85</fpage><lpage>96</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Манапова А.К., Бекетаева А.О., Макаров В.В., 2023</copyright-statement><copyright-year>2023</copyright-year><copyright-holder xml:lang="ru">Манапова А.К., Бекетаева А.О., Макаров В.В.</copyright-holder><copyright-holder xml:lang="en">Мanapova A., Beketaeva A., Makarov V.</copyright-holder><license xml:lang="ru" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>Данная работа распространяется под лицензией Creative Commons Attribution 4.0.</license-p></license><license xml:lang="en" license-type="creative-commons-attribution" xlink:href="https://creativecommons.org/licenses/by/4.0/" xlink:type="simple"><license-p>This work is licensed under a Creative Commons Attribution 4.0 License.</license-p></license></permissions><self-uri xlink:href="https://vestnik.kbtu.edu.kz/jour/article/view/877">https://vestnik.kbtu.edu.kz/jour/article/view/877</self-uri><abstract><p>Предлагается новый метод решения существенно дозвуковых течений, который представляет собой значительный шаг в области численного моделирования течений на основе системы уравнений Навье-Стокса. В методе используется ENO (Essentially Non-Oscillatory) схема третьего порядка точности, которая обеспечивает более высокую точность при расчетах течений с низкой скоростью звука. Одной из ключевых особенностей этого метода является введение параметров обезразмеривания. Эти параметры позволяют адаптировать уравнения Навье-Стокса к различным физическим условиям и избежать жесткости уравнений, что часто встречается в задачах численного моделирования. Это делает метод более гибким и применимым к разнообразным инженерным и физическим задачам. Для проверки и апробации данной методики проводятся вычисления для двух важных задач – течения внутри каверны и течения Пуазейля. Рассматривается значение числа Рейнольдса, Re=100, а также различные размеры вычислительных сеток. Полученные результаты сравниваются с экспериментальными данными, и наблюдается высокая степень согласования между моделью и реальными явлениями. Это свидетельствует об эффективности и точности предложенного метода в решении сложных течений в различных инженерных и физических задачах.</p></abstract><trans-abstract xml:lang="en"><p>A new method for solving essentially subsonic flows is proposed, which represents a significant step in the field of numerical modeling of flows based on the Navier-Stokes system of equations. The method uses an ENO (Essentially Non-Oscillatory) scheme of third order accuracy, which provides higher accuracy when calculating flows with low speed of sound. One of the key features of this method is the introduction of nondimensionalization parameters. These parameters make it possible to adapt the Navier-Stokes equations to different physical conditions and avoid the rigidity of the equations, which is often encountered in numerical modeling problems. This makes the method more flexible and applicable to a variety of engineering and physical problems. To check and approbate this technique, calculations are carried out for two important problems - flow inside a cavern and Poiseuille flow. The value of the Reynolds number, Re=100, as well as various sizes of computational grids are considered. The obtained results are compared with experimental data, and a high degree of agreement between the model and real phenomena is observed. This indicates the effectiveness and accuracy of the proposed method in solving complex flows in various engineering and physical problems.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>сжимаемый газ</kwd><kwd>уравнения Навье-Стокса</kwd><kwd>обезразмеривание</kwd><kwd>каверна</kwd><kwd>течение Пуазейля</kwd><kwd>число Маха</kwd></kwd-group><kwd-group xml:lang="en"><kwd>compressible gas</kwd><kwd>Navier-Stokes equations</kwd><kwd>dimensionlessness</kwd><kwd>cavity</kwd><kwd>Poiseuille flow</kwd><kwd>Mach number</kwd></kwd-group></article-meta></front><back><ref-list><title>References</title><ref id="cit1"><label>1</label><citation-alternatives><mixed-citation xml:lang="ru">Karki K., Patankar S. V. Pressure based calculation procedure for viscous flows at all speeds in arbitrary configurations. AIAA journal, vol. 27, no. 9, pp. 1167–1174.</mixed-citation><mixed-citation xml:lang="en">Karki K., Patankar S. V. 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