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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-325</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>Расчетное исследование взаимодействия реактивной струи с отклоняющим щитом</article-title><trans-title-group xml:lang="en"><trans-title>Computer modeling of exhaust jet flux interaction with deflecting shield</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>Картышев</surname><given-names>О. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Kartishev</surname><given-names>O. A.</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>ГосНИИ ГА</institution><country>Russian Federation</country></aff><pub-date pub-type="collection"><year>2014</year></pub-date><pub-date pub-type="epub"><day>07</day><month>11</month><year>2016</year></pub-date><volume>0</volume><issue>208</issue><fpage>54</fpage><lpage>59</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Картышев О.А., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Картышев О.А.</copyright-holder><copyright-holder xml:lang="en">Kartishev O.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://avia.mstuca.ru/jour/article/view/325">https://avia.mstuca.ru/jour/article/view/325</self-uri><abstract><p>В статье изложены методика и результаты расчетного исследования взаимодействия выхлопной реактивной струи со струеотклоняющим щитом. Работа направлена на решение конкретной экологической задачи - снижение воздействия шума на технический персонал аэропорта и пассажиров. В основу решения задачи положена система осредненных уравнений Рейнольдса, для решения которой используется метод контрольного объема.</p></abstract><trans-abstract xml:lang="en"><p>Method of exhaust jet flux interaction with deflecting shield computer modeling is proposed in this article. The article is devoted to concrete ecological task - to decrease the noise influence on ground maintenance stuff and passengers in the airports. The method is based on the Reynolds equation system solution obtained with the help of control volume method. Calculation results give an opportunity to choose main deflecting shield parameters according to concrete airport conditions.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>реактивная струя</kwd><kwd>струеотклоняющие щиты</kwd><kwd>расчет течения</kwd><kwd>метод контрольного объема</kwd></kwd-group><kwd-group xml:lang="en"><kwd>jet flux</kwd><kwd>deflecting shield</kwd><kwd>computer flow modeling</kwd><kwd>method of definite volume</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">Абрамович Г.Н. Теория турбулентных струй. - М.: Физматгиз, 1960.</mixed-citation><mixed-citation xml:lang="en">Абрамович Г.Н. Теория турбулентных струй. - М.: Физматгиз, 1960.</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Абрамович Г.Н., Крашенинников С.Ю., Секундов А.Н., Смирнова И.П. Турбулентное смешение газовых струй. - М.: Наука, 1974.</mixed-citation><mixed-citation xml:lang="en">Абрамович Г.Н., Крашенинников С.Ю., Секундов А.Н., Смирнова И.П. Турбулентное смешение газовых струй. - М.: Наука, 1974.</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>
