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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">avroen</journal-id><journal-title-group><journal-title xml:lang="ru">Омский научный вестник. Серия "Авиационно-ракетное и энергетическое машиностроение"</journal-title><trans-title-group xml:lang="en"><trans-title>Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">2588-0373</issn><issn pub-type="epub">2587-764X</issn><publisher><publisher-name>Омский государственный технический университет</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.25206/2588-0373-2024-8-3-98-106</article-id><article-id custom-type="edn" pub-id-type="custom">BVJEFS</article-id><article-id custom-type="elpub" pub-id-type="custom">avroen-68</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>АВИАЦИОННАЯ И РАКЕТНО-КОСМИЧЕСКАЯ ТЕХНИКА</subject></subj-group><subj-group subj-group-type="section-heading" xml:lang="en"><subject>AVIATION AND ROCKET-SPACE ENGINEERING</subject></subj-group></article-categories><title-group><article-title>Теоретико-экспериментальные исследования влияния параметров газового потока на унос капель жидкости из экспериментальной ёмкости</article-title><trans-title-group xml:lang="en"><trans-title>Theoretical and experimental studies of the influence of gas flow parameters on the entrainment of liquid droplets from an experimental vessel</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><contrib-id contrib-id-type="orcid">https://orcid.org/0000-0002-8837-7050</contrib-id><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Урбанский</surname><given-names>В. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Urbansky</surname><given-names>V. A.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Урбанский Владислав Александрович, кандидат технических наук, младший научный сотрудник НИЛ «Проектирование специальных бортовых систем ракет-носителей и космических аппаратов», ассистент кафедры «Авиа- и ракетостроение» </p><p>644050, г. Омск, пр. Мира, 11</p><p>AuthorID (SCOPUS): 57214753501</p></bio><bio xml:lang="en"><p>Urbansky Vladislav  Aleksandrovich,  Candidate of Technical Sciences, Junior Researcher of Design of Special on-board Systems of Launch Vehicles and Spacecraft’s Research Laboratory, Assistant of Aircraft and Rocket Building Department</p><p>Omsk, Mira Ave., 11, 644050</p><p>AuthorID (SCOPUS): 57214753501</p><p> </p></bio><email xlink:type="simple">vladurba95@gmail.com</email><xref ref-type="aff" rid="aff-1"/></contrib><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Петрук</surname><given-names>А. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Petruk</surname><given-names>A. A.</given-names></name></name-alternatives><bio xml:lang="ru"><p>Петрук Антон Андреевич, инженер НИЛ «Проектирование специальных бортовых систем ракет-носителей и космических аппаратов»</p><p>644050, г. Омск, пр. Мира, 11</p><p> </p><p> </p></bio><bio xml:lang="en"><p>Petruk Anton Andreevich, Engineer of Design of Special on-board Systems of Launch Vehicles and Spacecraft’s Research Laboratory</p><p>Omsk, Mira Ave., 11, 644050</p></bio><email xlink:type="simple">apetruk1800@gmail.com</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff-alternatives id="aff-1"><aff xml:lang="ru">Омский государственный технический университет<country>Россия</country></aff><aff xml:lang="en">Omsk State Technical University<country>Russian Federation</country></aff></aff-alternatives><pub-date pub-type="collection"><year>2024</year></pub-date><pub-date pub-type="epub"><day>30</day><month>09</month><year>2024</year></pub-date><volume>8</volume><issue>3</issue><fpage>98</fpage><lpage>106</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Урбанский В.А., Петрук А.А., 2024</copyright-statement><copyright-year>2024</copyright-year><copyright-holder xml:lang="ru">Урбанский В.А., Петрук А.А.</copyright-holder><copyright-holder xml:lang="en">Urbansky V.A., Petruk A.A.</copyright-holder><license 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://ariem.omgtu.ru/jour/article/view/68">https://ariem.omgtu.ru/jour/article/view/68</self-uri><abstract><p>На основе математического моделирования получены значения скоростей над поверхностью жидкости в экспериментальной ёмкости для обеспечения условия отрыва и уноса капель. Разработана программа физических экспериментов по уносу капель жидкости из экспериментальной ёмкости. Проведено физическое моделирование уноса капель жидкости из экспериментальной ёмкости, которое показало, что процент отделения жидкой фазы сепаратором увеличивается с увеличением температурного режима входного газового потока. При температуре входного газового потока равной 20 ºС процент отделения составил 62 %, при 30 ºС — 69 %, при 35 ºС — 70 %, при 40 ºС — 78 %.</p></abstract><trans-abstract xml:lang="en"><p>On the basis of mathematical modeling, the values of velocities above the liquid surface in the experimental vessel are obtained to ensure the condition of droplet detachment and entrainment. The program of physical experiments on the entrainment of liquid droplets from experimental vessel is developed. Physical modeling of liquid droplets entrainment from experimental vessel is carried out, which showed that the separated mass of liquid significantly depends on the parameters of the gas flow at the inlet to experimental vessel (temperature, flow velocity). At the temperature of the inlet gas flow equal to 20 °C the percentage of separation ts 62 %, at 30 ºC — 69 %, at 35 ºC — 70 %, at 40 ºC — 78 %.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>центробежный сепаратор</kwd><kwd>капли жидкости</kwd><kwd>скорость газового потока</kwd><kwd>критерии подобия</kwd><kwd>параметры газового потока</kwd><kwd>двухфазный поток</kwd><kwd>унос капель жидкости</kwd><kwd>пассивация</kwd></kwd-group><kwd-group xml:lang="en"><kwd>centrifugal separator</kwd><kwd>liquid droplets</kwd><kwd>gas flow velocity</kwd><kwd>similarity criteria</kwd><kwd>gas flow parameters</kwd><kwd>two-phase flow</kwd><kwd>liquid droplet entrainment</kwd><kwd>passivation</kwd></kwd-group><funding-group xml:lang="ru"><funding-statement>Исследование выполнено за счет гранта Российского научного фонда № 23-29-00531</funding-statement></funding-group><funding-group xml:lang="en"><funding-statement>The research is funded by the Russian Science Foundation No. 23-29-00531</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">ГОСТ Р. 52925-2018. 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