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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-127</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>К вопросу определения геометрии крыла транспортного воздушного судна в полете</article-title><trans-title-group xml:lang="en"><trans-title>DETERMINATION OF COMMERCIAL AIRCRAFT WING GEOMETRY DURING THE FLIGHT</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>Шевяков</surname><given-names>В. И.</given-names></name><name name-style="western" xml:lang="en"><surname>Shevyakov</surname><given-names>V. I.</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>ЗАО "Гражданские самолеты Сухого"</institution><country>Russian Federation</country></aff><pub-date pub-type="collection"><year>2015</year></pub-date><pub-date pub-type="epub"><day>07</day><month>11</month><year>2016</year></pub-date><issue>212</issue><fpage>60</fpage><lpage>65</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Шевяков В.И., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Шевяков В.И.</copyright-holder><copyright-holder xml:lang="en">Shevyakov V.I.</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/127">https://avia.mstuca.ru/jour/article/view/127</self-uri><abstract><p>Рассматривается задача определения фотограмметрическим методом формы крыла дозвуковых транспортных ВС. Излагается методика проведения измерений на земле и в полете. Представлены результаты измерений крутки крыла транспортного ВС на крейсерском режиме полета.</p></abstract><trans-abstract xml:lang="en"><p>The article deals with the task of determination of wing shape for sub-sonic commercial aircraft by photogrammetric method. It provides the procedure for measurements taken on ground and in flight. It also provides the outcome of wing twist for commercial aircraft at cruise.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>воздушное судно</kwd><kwd>крутка крыла</kwd><kwd>фотограмметрический метод</kwd></kwd-group><kwd-group xml:lang="en"><kwd>aircraft</kwd><kwd>wing twist</kwd><kwd>photogrammetric method</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">Кулеш В.П., Фонов С.Д. Измерение параметров движения и деформации модели самолета в аэродинамической трубе методом видеограмметрии // Ученые записки ЦАГИ. 1998. Т. XXIX. № 1-2. С. 165-176.</mixed-citation><mixed-citation xml:lang="en">Polsky S.A. A computational study of unsteady ship airwake. AIAA 2002-1022. 2002. P. 11.</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Кулеш В.П. Бесконтактные измерения геометрических параметров формы, движения и деформации объектов в экспериментальной аэродинамике // Датчики и системы. 2004. № 3. С. 22-27.</mixed-citation><mixed-citation xml:lang="en">Bobylev A.V., Vyshinsky V.V., Soudakov G.G., Yaroshevsky V.A. Aircraft Vortex Wake and Flight Safety Problems. Journal of Aircraft. Vol. 47. № 2. March–April 2010.</mixed-citation></citation-alternatives></ref><ref id="cit3"><label>3</label><citation-alternatives><mixed-citation xml:lang="ru">Kulesh V.P., Bosnyakov S.M., Bykov A.P. Blade Deformation and PSP Measurements on Large Scale Rotor by Video metric System, ICIASF’97 Record, Sept. 29 - Oct. 2, 1997, IEEE Publication 97CH36121. Pp. 95-103.</mixed-citation><mixed-citation xml:lang="en">Vihshinskiyj V.V., Sudakov G.G. Vihrevoj sled samoleta v turbulentnoj atmosphere. Trudih CAGI. 2005. Vihp. 2667. P. 155. (In Russian).</mixed-citation></citation-alternatives></ref><ref id="cit4"><label>4</label><citation-alternatives><mixed-citation xml:lang="ru">Долотовский А.В., Шевяков В.И. Результаты использования фотограмметрического метода для определения геометрических параметров крыла самолета SSJ-100 / Материалы XXV науч.-техн. конф. по аэродинамике. М.: ЦАГИ, 2014. С. 116-117.</mixed-citation><mixed-citation xml:lang="en">Garbaruk A.V., Strelec M.Kh., Shur M.L. Modelirovanie turbulentnosti v raschetakh slozhnihkh techeniyj: uchebnoe posobie. SPb.: Izd-vo Politekhn. un-ta. 2012. 88 p. (In Russian).</mixed-citation></citation-alternatives></ref><ref id="cit5"><label>5</label><citation-alternatives><mixed-citation xml:lang="ru">Landau L.D., Lifshic E.M. Teoreticheskaya fizika. Gidrodinamika. M.: Nauka. 1988. T. 6. 736 p. (In Russian).</mixed-citation><mixed-citation xml:lang="en">Landau L.D., Lifshic E.M. Teoreticheskaya fizika. Gidrodinamika. M.: Nauka. 1988. T. 6. 736 p. (In Russian).</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>
