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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">ntv</journal-id><journal-title-group><journal-title xml:lang="ru">Научно-технический вестник информационных технологий, механики и оптики</journal-title><trans-title-group xml:lang="en"><trans-title>Scientific and Technical Journal of Information Technologies, Mechanics and Optics</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">2226-1494</issn><issn pub-type="epub">2500-0373</issn><publisher><publisher-name>Университет ИТМО</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.17586/2226-1494-2025-25-1-140-150</article-id><article-id custom-type="elpub" pub-id-type="custom">ntv-429</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>МАТЕМАТИЧЕСКОЕ И КОМПЬЮТЕРНОЕ МОДЕЛИРОВАНИЕ</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>MODELING AND SIMULATION</subject></subj-group></article-categories><title-group><article-title>Моделирование износа алюминиевого сплава частицами SiO2</article-title><trans-title-group xml:lang="en"><trans-title>Numerical study of SiO2 particle erosion of an aluminum alloy</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0001-5376-1231</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Строкач</surname><given-names>Е. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Strokach</surname><given-names>E. A.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Строкач Евгений Александрович — кандидат технических наук, ведущий инженер</p><p>Москва, 125993</p></bio><bio xml:lang="en"><p>Evgeny A. Strokach — PhD, Leading Engineer</p><p>Moscow, 125993</p></bio><email xlink:type="simple">evgenij.strokatsch@mai.ru</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0002-7667-5392</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Пожидаев</surname><given-names>А. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Pozhidaev</surname><given-names>A. A.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Пожидаев Алексей Алексеевич — ассистент</p><p>Москва, 125993</p></bio><bio xml:lang="en"><p>Alexei A. Pozhidaev — Assistant</p><p>Moscow, 125993</p></bio><email xlink:type="simple">aapozhidaev@mai.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru"><institution>Московский авиационный институт (национальный исследовательский университет)</institution><country>Россия</country></aff><aff xml:lang="en"><institution>Moscow Aviation Institute (National Research University)</institution><country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2025</year></pub-date><pub-date pub-type="epub"><day>28</day><month>02</month><year>2025</year></pub-date><volume>25</volume><issue>1</issue><fpage>140</fpage><lpage>150</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Строкач Е.А., Пожидаев А.А., 2025</copyright-statement><copyright-year>2025</copyright-year><copyright-holder xml:lang="ru">Строкач Е.А., Пожидаев А.А.</copyright-holder><copyright-holder xml:lang="en">Strokach E.A., Pozhidaev A.A.</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://ntv.elpub.ru/jour/article/view/429">https://ntv.elpub.ru/jour/article/view/429</self-uri><abstract><p>Введение. Современные методы моделирования процесса эрозии материалов твердыми частицами позволяют на микроуровне оценить влияние условий движения частиц, контакта с поверхностью, их формы и материала. Известные зарубежные работы по изучению пар эродента и алюминиевых, титановых сплавов и сталей не дают правильной оценки влияния трения и вращения частиц на остаточное напряженно-деформированное состояние и глубину износа при относительно высоких скоростях частиц. Мало изученным остается вопрос кратковременного нагрева приповерхностного слоя, что при высоких температурах может влиять на свойства материала. Устранение такой неопределенности повысит предиктивную точность модели абразивного износа. Метод. В работе представлены результаты двумерного конечно-элементного моделирования эрозионного износа поверхности распространенного алюминиевого сплава Al6061-T6 при взаимодействии с частицами двуокиси кремния (SiO2). Упругопластическое поведение материала поверхности и условия разрушения задавались моделью Джонсона–Кука. Основные результаты. Для оценки взаимовлияния следов множественных ударов частиц и изменения напряженно-деформированного состояния поверхности выполнено моделирование последовательных ударов трех групп жестких частиц диаметром 250 мкм со скоростью 155 м/с под углом 45°. Изучено изменение эквивалентных напряжений в образце после каждого удара. Проведена оценка влияния трения между частицами SiO2 и поверхностью, а также вращения сферических частиц и его направления. Обсуждение. Показано, что учет трения влияет на профиль эквивалентных напряжений уже после первого удара и сохраняет влияние в дальнейшем. Зависимость результатов от направления вращения частиц при скорости 1000 об/мин проявляется только после второго удара и усиливается после удара третьей группы частиц. Предполагается, что для алюминиевых сплавов серии 6000 и сферических частиц SiO2 другого размера полученные зависимости будут качественно сохраняться. Дальнейшие исследования предполагают анализ влияния формы несферических частиц SiO2 при вращении, важность учета деформируемости частиц при ударе, а также воздействие этих эффектов при большем количестве ударов и различных условиях контакта.</p></abstract><trans-abstract xml:lang="en"><p>Computational methods used to simulate solid particle erosion have advanced so far being able to estimate partial effect of various processing factors on microlevel, such as particle-surface contact, its particle material, and shape, etc. The published activities taken to study different effects in this aspect for popular aluminium or titanium alloys and steels still have a gap in knowledge addressing some process parameters. The influence of particle rotation and its direction on stress-strain state and wear depth is still understudied. The impact of friction consideration in relatively high-speed contacts should also be studied, as well as the surface layer heating effect which may influence the material strength properties when the temperatures get high. Understanding these effects would increase the predictive ability of the erosion model and its accuracy — which is presented in our 2D simulation study for SiO2 solid particles and a widespread Al6061-T6 alloy. The elastic-plastic and failure properties of the surface material were presented by the Johnson-Cook model. To estimate the influence of multiple impacts on the stress-strain state, three sequential rigid impacts of 250 µm particles at 45° and 155 m/s were modeled. Main attention was driven to the evolution of equivalent von-Mises stresses in the sample after each impact and its dependence on the friction and rotation of particles. It was shown that the effect of friction can be noticed after the first impact, remaining high throughout the simulation. Whereas the influence of rotation direction at 1000 rpm was noticeable after the second impact and tended to increase after the third impact. It is assumed that for other 6000 series aluminium alloys being eroded by spherical SiO2 particles with differing diameters the erosive behavior would keep. However, future studies should be addressed to the analyzing of non-spherical particles rotation, consideration of particle deformation, and to studies of these parameters including more impacts and different contact properties in complex.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>эрозия твердыми частицами</kwd><kwd>абразивный износ</kwd><kwd>FEA-моделирование эрозии</kwd><kwd>ANSYS Explicit</kwd><kwd>остаточные  напряжения</kwd><kwd>модель Джонсона–Кука</kwd><kwd>Al6061</kwd></kwd-group><kwd-group xml:lang="en"><kwd>solid particle erosion</kwd><kwd>abrasive wear</kwd><kwd>FEA erosion simulation</kwd><kwd>ANSYS Explicit</kwd><kwd>residual stresses</kwd><kwd>Johnson-Cook model</kwd><kwd>Al6061</kwd></kwd-group><funding-group><funding-statement xml:lang="ru">Работа выполнена в рамках государственного задания Министерства науки и высшего образования Российской  Федерации, тема № FSFF-2023-0006.</funding-statement><funding-statement xml:lang="en">The work was funded by the Ministry of Science and Higher Education of the Russian Federation, grant No. FSFF-2023-0006.</funding-statement></funding-group></article-meta></front><back><ref-list><title>References</title><ref id="cit1"><label>1</label><citation-alternatives><mixed-citation xml:lang="ru">Боркова А.Н. 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