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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">10.55452/1998-6688-2024-21-2-193-206</article-id><article-id custom-type="elpub" pub-id-type="custom">kaz29-1266</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>МЕТОД ПРЕДОБУСЛАВЛИВАНИЯ ДЛЯ СУЩЕСТВЕННО ДОЗВУКОВЫХ ПОТОКОВ</article-title><trans-title-group xml:lang="en"><trans-title>PRE-CONDITIONING METHOD FOR SUBSTANTIALLY SUBSONIC FLOWS</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>магистр прикладной математики и информатики</p><p>050039, г. Алматы</p></bio><bio xml:lang="en"><p>Master of applied mathematics and computer science</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>д-р.физ.-мат.наук</p><p>050010, г. Алматы</p></bio><bio xml:lang="en"><p>Dr. Phys.-Math. Sc.</p><p>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>канд. техн. наук.</p><p>117997, г. Москва</p><p>115409, г. Москва</p></bio><bio xml:lang="en"><p>Can. Tech. Sc.</p><p>117997, Moscow</p><p>115409, 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">Академия 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»; National research nuclear university «MEPhI»<country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2024</year></pub-date><pub-date pub-type="epub"><day>02</day><month>07</month><year>2024</year></pub-date><volume>21</volume><issue>2</issue><fpage>193</fpage><lpage>206</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Манапова А.К., Бекетаева А.О., Макаров В.В., 2024</copyright-statement><copyright-year>2024</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/1266">https://vestnik.kbtu.edu.kz/jour/article/view/1266</self-uri><abstract><p>Предлагаемая работа представляет собой детальное численное моделирование трехмерного дозвукового турбулентного течения в канале с основным упором на симметричные перпендикулярные струи, возникающие у стенок. Решение осредненных по Фавру уравнений Навье-Стокса, замкнутых моделью турбулентности, осуществляется с помощью алгоритма, основанного на схеме ENO. Для ускорения сходимости итерационного процесса используется метод предобуславливания и осуществляется переход к вектору примитивных переменных. Результаты исследования важны для лучшего понимания дозвуковых турбулентных потоков и могут найти применение в различных областях, включая инженерные и научные исследования. Актуальность работы подчеркивается разработкой эффективных численных алгоритмов, позволяющих решать дозвуковые трехмерные уравнения Навье-Стокса с использованием схем высокого порядка точности, а также с применением робастных моделей турбулентности для анализа сверхзвукового многокомпонентного течения. Научная новизна работы заключается в успешном использовании метода предобусловливания для ускорения сходимости итерационного процесса.</p></abstract><trans-abstract xml:lang="en"><p>The proposed work is a detailed numerical simulation of three-dimensional subsonic turbulent flow in a channel, with the main focus on symmetric perpendicular jets arising from the walls. The solution of the Favreaveraged Navier-Stokes equations closed by the turbulence model is carried out using an algorithm based on the ENO scheme. To accelerate the convergence of the iterative process, a preconditioning method is used and a transition to a vector of primitive variables is performed. The results of the study are essential for a better understanding of subsonic turbulent flows and may find applications in various fields, including engineering and scientific research. The relevance of the work is highlighted by the development of efficient numerical algorithms capable of solving subsonic three-dimensional Navier-Stokes equations using high-order accuracy schemes, as well as the application of robust turbulence models to analyze supersonic multicomponent flow. The scientific novelty of the work is the successful use of the preconditioning method to accelerate the convergence of the iterative process.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>численное моделирование</kwd><kwd>дозвуковое течение</kwd><kwd>идеальный газ</kwd><kwd>пограничный слой</kwd><kwd>уравнения Навье-Стокса</kwd></kwd-group><kwd-group xml:lang="en"><kwd>numerical modelling</kwd><kwd>subsonic flow</kwd><kwd>perfect gas</kwd><kwd>boundary layer</kwd><kwd>Navier-Stokes equations</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">Volkov K.N. (2009) Pre-conditioning of the Euler and Navier-Stokes equations in modeling of low-speed flows on unreconstructed meshes. Computational Mathematics and Mathematical Physics., vol. 49, no. 10, pp. 1868–1884.</mixed-citation><mixed-citation xml:lang="en">Volkov K.N. (2009) Pre-conditioning of the Euler and Navier-Stokes equations in modeling of low-speed flows on unreconstructed meshes. Computational Mathematics and Mathematical Physics., vol. 49, no. 10, pp. 1868–1884.</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Geiser G., Wellner J., Ku ̈geler E., Weber A., Moors A. (2019) On the simulation and spectral analysis of unsteady turbulence and transition effects in a multistage low pressure turbine.</mixed-citation><mixed-citation xml:lang="en">Geiser G., Wellner J., Ku ̈geler E., Weber A., Moors A. (2019) On the simulation and spectral analysis of unsteady turbulence and transition effects in a multistage low pressure turbine.</mixed-citation></citation-alternatives></ref><ref id="cit3"><label>3</label><citation-alternatives><mixed-citation xml:lang="ru">Chen S., Cai F., Xiang X., Gao Z., Yan C. (2021) A low-diffusion robust flux splitting scheme towards wide-ranging Mach number flows. Chinese J Aeronaut, no. 34(5), pp. 628–41.</mixed-citation><mixed-citation xml:lang="en">Chen S., Cai F., Xiang X., Gao Z., Yan C. (2021) A low-diffusion robust flux splitting scheme towards wide-ranging Mach number flows. Chinese J Aeronaut, no. 34(5), pp. 628–41.</mixed-citation></citation-alternatives></ref><ref id="cit4"><label>4</label><citation-alternatives><mixed-citation xml:lang="ru">Redchyts D., Fernandez-Gamiz U., Polevoy O., Moiseienko S., Portal-Porras K. (2023) Numerical simulation of subsonic flow around oscillating airfoil based on the Navier-Stokes equations. Energy Sources, Part A: Recovery, Utilization, and Environmental Effects, vol. 45, pp. 9993–10009.</mixed-citation><mixed-citation xml:lang="en">Redchyts D., Fernandez-Gamiz U., Polevoy O., Moiseienko S., Portal-Porras K. (2023) Numerical simulation of subsonic flow around oscillating airfoil based on the Navier-Stokes equations. Energy Sources, Part A: Recovery, Utilization, and Environmental Effects, vol. 45, pp. 9993–10009.</mixed-citation></citation-alternatives></ref><ref id="cit5"><label>5</label><citation-alternatives><mixed-citation xml:lang="ru">Choi D., Merkle C.L. (986) Application of the establishment method for the calculation of low-speed flows. Aerospace Engineering, no. 7, pp. 29–37.</mixed-citation><mixed-citation xml:lang="en">Choi D., Merkle C.L. (986) Application of the establishment method for the calculation of low-speed flows. Aerospace Engineering, no. 7, pp. 29–37.</mixed-citation></citation-alternatives></ref><ref id="cit6"><label>6</label><citation-alternatives><mixed-citation xml:lang="ru">Strelets M. X., Shur M. (1988) A method of compressibility scaling for calculation of stationary viscous gas flows at arbitrary Mach numbers. ZhVM and MF, vol. 28, pp. 254–266.</mixed-citation><mixed-citation xml:lang="en">Strelets M. X., Shur M. (1988) A method of compressibility scaling for calculation of stationary viscous gas flows at arbitrary Mach numbers. ZhVM and MF, vol. 28, pp. 254–266.</mixed-citation></citation-alternatives></ref><ref id="cit7"><label>7</label><citation-alternatives><mixed-citation xml:lang="ru">Turkel E. (1987) Preconditioned Method for Solving the Incompressible and Low Speed Compressible Equations. J.of Comp.Physics., vol. 72, pp. 277–298.</mixed-citation><mixed-citation xml:lang="en">Turkel E. (1987) Preconditioned Method for Solving the Incompressible and Low Speed Compressible Equations. J.of Comp.Physics., vol. 72, pp. 277–298.</mixed-citation></citation-alternatives></ref><ref id="cit8"><label>8</label><citation-alternatives><mixed-citation xml:lang="ru">Tomboulides A.G. and Orzag S.A. (1998) A quasi-two-dimensional benchmark problem for low Mach number compressible codes. J.Comp. Phys., vol. 146, no. 2, pp. 691–706.</mixed-citation><mixed-citation xml:lang="en">Tomboulides A.G. and Orzag S.A. (1998) A quasi-two-dimensional benchmark problem for low Mach number compressible codes. J.Comp. Phys., vol. 146, no. 2, pp. 691–706.</mixed-citation></citation-alternatives></ref><ref id="cit9"><label>9</label><citation-alternatives><mixed-citation xml:lang="ru">Maia A., Silva J.F., Tomita J.T., Bringhenti C. Applying a Preconditioning Technique to the Euler Equations to Accelerate the Convergence Rate for Low-Speed Flows. Proceedings of the 5th World Congress on Mechanical, Chemical, and Material Engineering (MCM'19), 2019.</mixed-citation><mixed-citation xml:lang="en">Maia A., Silva J.F., Tomita J.T., Bringhenti C. Applying a Preconditioning Technique to the Euler Equations to Accelerate the Convergence Rate for Low-Speed Flows. Proceedings of the 5th World Congress on Mechanical, Chemical, and Material Engineering (MCM'19), 2019.</mixed-citation></citation-alternatives></ref><ref id="cit10"><label>10</label><citation-alternatives><mixed-citation xml:lang="ru">Dong H., Liu F. (2022) A new accelerating technique for low speed flow: pseudo high speed method. Chinese Journal of Aeronautics, no. 35 (8), pp. 45–64.</mixed-citation><mixed-citation xml:lang="en">Dong H., Liu F. (2022) A new accelerating technique for low speed flow: pseudo high speed method. Chinese Journal of Aeronautics, no. 35 (8), pp. 45–64.</mixed-citation></citation-alternatives></ref><ref id="cit11"><label>11</label><citation-alternatives><mixed-citation xml:lang="ru">Nguyen V., Park W. (2023) A Review of Preconditioning and Artificial Compressibility Dual-Time Navier–Stokes Solvers for Multiphase Flows. Fluids, no. 8, 100.</mixed-citation><mixed-citation xml:lang="en">Nguyen V., Park W. (2023) A Review of Preconditioning and Artificial Compressibility Dual-Time Navier–Stokes Solvers for Multiphase Flows. Fluids, no. 8, 100.</mixed-citation></citation-alternatives></ref><ref id="cit12"><label>12</label><citation-alternatives><mixed-citation xml:lang="ru">Pierre S., Christian F., Edmund K., Markus K. Low Mach preconditioning for turbomachinery flow simulations with cavities and variable gas compositions. Proceedings of ASME Turbo Expo, 2022.</mixed-citation><mixed-citation xml:lang="en">Pierre S., Christian F., Edmund K., Markus K. Low Mach preconditioning for turbomachinery flow simulations with cavities and variable gas compositions. Proceedings of ASME Turbo Expo, 2022.</mixed-citation></citation-alternatives></ref><ref id="cit13"><label>13</label><citation-alternatives><mixed-citation xml:lang="ru">Maia A., Kapat J. Tomita J.T., Silva J.F., Bringhenti C., Cavalca D. Preconditioning methods for compressible flow CFD codes: Revisited. International Journal of Mechanical Sciences, 2020.</mixed-citation><mixed-citation xml:lang="en">Maia A., Kapat J. Tomita J.T., Silva J.F., Bringhenti C., Cavalca D. Preconditioning methods for compressible flow CFD codes: Revisited. International Journal of Mechanical Sciences, 2020.</mixed-citation></citation-alternatives></ref><ref id="cit14"><label>14</label><citation-alternatives><mixed-citation xml:lang="ru">Hongyuan L., Chongwen J., Shuyao H., Zhenxuan G., Chun-Hian L. (2023) Disturbance region update method with preconditioning for steady compressible and incompressible flows. Computer Physics Communications, vol. 285.</mixed-citation><mixed-citation xml:lang="en">Hongyuan L., Chongwen J., Shuyao H., Zhenxuan G., Chun-Hian L. (2023) Disturbance region update method with preconditioning for steady compressible and incompressible flows. Computer Physics Communications, vol. 285.</mixed-citation></citation-alternatives></ref><ref id="cit15"><label>15</label><citation-alternatives><mixed-citation xml:lang="ru">Beketaeva A.O. (2007) Application of eno-scheme (essentially nonoscillatory) for modeling the flow of multicomponent gas mixture. Computational Technologies, Nosibirsk, vol. 12, no. S4, pp. 17–25.</mixed-citation><mixed-citation xml:lang="en">Beketaeva A.O. (2007) Application of eno-scheme (essentially nonoscillatory) for modeling the flow of multicomponent gas mixture. Computational Technologies, Nosibirsk, vol. 12, no. S4, pp. 17–25.</mixed-citation></citation-alternatives></ref><ref id="cit16"><label>16</label><citation-alternatives><mixed-citation xml:lang="ru">Wilcox D.C. Turbulence modeling for CFD: DCW Industries Inc., 1993, p. 460.</mixed-citation><mixed-citation xml:lang="en">Wilcox D.C. Turbulence modeling for CFD: DCW Industries Inc., 1993, p. 460.</mixed-citation></citation-alternatives></ref><ref id="cit17"><label>17</label><citation-alternatives><mixed-citation xml:lang="ru">Thompson K.W. (1987) Time dependent boundary conditions for hyperbolic systems. J.Comp. Phys., no. 2, pp. 1–24.</mixed-citation><mixed-citation xml:lang="en">Thompson K.W. (1987) Time dependent boundary conditions for hyperbolic systems. J.Comp. Phys., no. 2, pp. 1–24.</mixed-citation></citation-alternatives></ref><ref id="cit18"><label>18</label><citation-alternatives><mixed-citation xml:lang="ru">Мanapova A., Beketaeva A., Makarov V. (2023) Numerical modeling of essentially subsonic flows of compressible gas. Herald of the Kazakh-British technical university, no.20(4), pp. 85–96 (In Russ.).</mixed-citation><mixed-citation xml:lang="en">Мanapova A., Beketaeva A., Makarov V. (2023) Numerical modeling of essentially subsonic flows of compressible gas. Herald of the Kazakh-British technical university, no.20(4), pp. 85–96 (In Russ.).</mixed-citation></citation-alternatives></ref><ref id="cit19"><label>19</label><citation-alternatives><mixed-citation xml:lang="ru">Poinsot T.J., Lele S.K. (1992) Boundary Conditions for Direct Simulations of Compressible Viscous Flows. Journal of Computational Physics, vol. 101, pp. 104–129.</mixed-citation><mixed-citation xml:lang="en">Poinsot T.J., Lele S.K. (1992) Boundary Conditions for Direct Simulations of Compressible Viscous Flows. Journal of Computational Physics, vol. 101, pp. 104–129.</mixed-citation></citation-alternatives></ref></ref-list><fn-group><fn fn-type="conflict"><p>The authors declare that there are no conflicts of interest present.</p></fn></fn-group></back></article>
