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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-263</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>ВИХРЕВАЯ ПОДЪЕМНО-ТРАНСПОРТНАЯ СИСТЕМА</article-title><trans-title-group xml:lang="en"><trans-title>VORTEX LIFTING AND TRANSPORTATION SYSTEM</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>Михненков</surname><given-names>Л. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Mihnenkov</surname><given-names>L. V.</given-names></name></name-alternatives><bio xml:lang="ru"><p>доктор технических наук, академик Российской академии космонавтики им. К.Э. Циолковского, профессор кафедры технической механики и инженерной графики МГТУ ГА</p></bio><email xlink:type="simple">Michnenkov@mstuca.ru</email><xref ref-type="aff" rid="aff-1"/></contrib></contrib-group><aff xml:lang="ru" id="aff-1"><institution>МГТУ ГА</institution><country>Russian Federation</country></aff><pub-date pub-type="collection"><year>2016</year></pub-date><pub-date pub-type="epub"><day>07</day><month>11</month><year>2016</year></pub-date><issue>223</issue><fpage>131</fpage><lpage>139</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Михненков Л.В., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Михненков Л.В.</copyright-holder><copyright-holder xml:lang="en">Mihnenkov L.V.</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/263">https://avia.mstuca.ru/jour/article/view/263</self-uri><abstract><p>Представлены результаты расчетного исследования подъемно-транспортной системы (ПТС) самолета вертикального взлета и посадки, базирующейся на использовании эффекта Магнуса. Получены формулы для определения ее подъемной силы и тяги. Разработан метод инженерного расчета основных элементов системы с учетом данных экспериментальных аэродинамических продувок.</p></abstract><trans-abstract xml:lang="en"><p>The results of numerical research of lifting and transport system of aircraft vertical takeoff and landing, based on the use of the Magnus effect are presented. The formulas for determining its lift and thrust are obtained. The method of engineering calculation of the basic elements of the system based on the data of experimental aerodynamic tests is developed.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>самолет. вертикальный взлет</kwd><kwd>посадка. подъемно-транспортная система. расчет</kwd></kwd-group><kwd-group xml:lang="en"><kwd>plane</kwd><kwd>vertical takeoff</kwd><kwd>vertical landing</kwd><kwd>lifting and transport system</kwd><kwd>calculation</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">Михненков Л.В. Авиационная подъемно-транспортная система и ветроэнергетические устройства вихревого типа: монография. - М.: МГТУ ГА. 2014. - 96 c.</mixed-citation><mixed-citation xml:lang="en">Mihnenkov L.V. Aviacionnaja podjomno-transportnaya sistema i wetrojenergeticheskie ustrojstva vihrevogo tipa. Monografiya. [Aviation lifting and transportation system and wind-energy devices of the vortex type. A monograph] Moscow. MGTUGA. 2014. 96 p.</mixed-citation></citation-alternatives></ref><ref id="cit2"><label>2</label><citation-alternatives><mixed-citation xml:lang="ru">Фабрикант Н.Я. Аэродинамика. Общий курс. - М.: Наука. 1964. - 815 с.</mixed-citation><mixed-citation xml:lang="en">Fabrikant N.Ya. Ajerodinamika obshhij kurs [Aerodynamics. General Course] Moscow. Nauka. 1964. 815 p.</mixed-citation></citation-alternatives></ref><ref id="cit3"><label>3</label><citation-alternatives><mixed-citation xml:lang="ru">Buseman A. Messungen an rotierenden Zylindern, Ergebn der Aerodyn. Versuchsanst. Zu Gőtt., IV, 101, 1932.</mixed-citation><mixed-citation xml:lang="en">A. Buseman. Messungen an rotierenden Zylindern, Ergebn der Aerodyn. Versuchsanst. Zu Gőtt., IV, 101, 1932.</mixed-citation></citation-alternatives></ref><ref id="cit4"><label>4</label><citation-alternatives><mixed-citation xml:lang="ru">Самойлович Г.С. Гидроаэромеханика: учебник для вузов по специальности "Турбиностроение" - М.: Машиностроение. 1980. - 280 с.</mixed-citation><mixed-citation xml:lang="en">Samojlovich G.S. Gidroajeromehanika. [Hydroaeromechanics: Textbook for universities in the specialty "turbine construction"] Moscow. Mashinostroenie. 1980. 280 p.</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>
