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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">caht</journal-id><journal-title-group><journal-title xml:lang="ru">Научный вестник МГТУ ГА</journal-title><trans-title-group xml:lang="en"><trans-title>Civil Aviation High Technologies</trans-title></trans-title-group></journal-title-group><issn pub-type="ppub">2079-0619</issn><issn pub-type="epub">2542-0119</issn><publisher><publisher-name>Moscow State Technical University of Civil Aviation (MSTU CA)</publisher-name></publisher></journal-meta><article-meta><article-id custom-type="elpub" pub-id-type="custom">caht-22</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>Статьи</subject></subj-group></article-categories><title-group><article-title>Численное моделирование процессов возникновения бафтинга для крыла ONERA M6</article-title><trans-title-group xml:lang="en"><trans-title>THE NUMERICAL SIMULATION OF THE BUFFETING'S APPEARANCE FOR ONERA M6 WING</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author" corresp="yes"><name-alternatives><name name-style="eastern" xml:lang="ru"><surname>Липатов</surname><given-names>И. И.</given-names></name><name name-style="western" xml:lang="en"><surname>Lipatov</surname><given-names>I. I.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.ru</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>Винь</surname><given-names>Ф. Т.</given-names></name><name name-style="western" xml:lang="en"><surname>Vinh</surname><given-names>P. T.</given-names></name></name-alternatives><email xlink:type="simple">noemail@neicon.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff xml:lang="ru" id="aff-1"><institution>МФТИ</institution><country>Russian Federation</country></aff><pub-date pub-type="collection"><year>2014</year></pub-date><pub-date pub-type="epub"><day>04</day><month>11</month><year>2016</year></pub-date><volume>0</volume><issue>200</issue><fpage>133</fpage><lpage>140</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Липатов И.И., Винь Ф.Т., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Липатов И.И., Винь Ф.Т.</copyright-holder><copyright-holder xml:lang="en">Lipatov I.I., Vinh P.T.</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://avia.mstuca.ru/jour/article/view/22">https://avia.mstuca.ru/jour/article/view/22</self-uri><abstract><p>Представлены результаты численного исследования возникновения бафтинга на крыле Onera M6. Определены границы возникновения режимов автоколебаний скачка уплотнения при взаимодействии с течением в пограничном слое по числам Маха и углам атаки.</p></abstract><trans-abstract xml:lang="en"><p>Introduction to the results of a numerical study buffeting on Onera M6 wing. The determination of condition to appear buffeting of the modes of oscillation of a shock when interacting with in the boundary layer at Mach numbers and angles of attack.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>трансзвуковое обтекание</kwd><kwd>автоколебания скачка уплотнения</kwd></kwd-group><kwd-group xml:lang="en"><kwd>transonic flow</kwd><kwd>oscillations of shock wave</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">Woodgate M.A. and Barakos G.N. (2012) Implicit computational fluid dynamics methods for fast analysis of rotor flows. AIAA Journal vol 50 issue 6 pp 1217-1244.</mixed-citation><mixed-citation xml:lang="en">Woodgate M.A. and Barakos G.N. (2012) Implicit computational fluid dynamics methods for fast analysis of rotor flows. AIAA Journal vol 50 issue 6 pp 1217-1244.</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Smagorinsky J. 1971: Numerical simulation of climate modification. In, Proceedings of the 12th Interagency Conference on Climate Modification, Virginia Beach, VA, 221-2263 [Электронный ресурс]. URL: http://www.aero.polimi.it/freecase/ ONERA-M6-wing.</mixed-citation><mixed-citation xml:lang="en">Smagorinsky J. 1971: Numerical simulation of climate modification. In, Proceedings of the 12th Interagency Conference on Climate Modification, Virginia Beach, VA, 221-2263 [Электронный ресурс]. URL: http://www.aero.polimi.it/freecase/ ONERA-M6-wing.</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>
