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<!DOCTYPE article PUBLIC "-//NLM//DTD JATS (Z39.96) Journal Publishing DTD v1.3 20210610//EN" "JATS-journalpublishing1-3.dtd">
<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-268</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>ШАССИ НА ВОЗДУШНОЙ ПОДУШКЕ С МНОГОСЕКЦИОННЫМ ФОРМИРОВАНИЕМ ВОЗДУШНОЙ ПОДУШКИ ДЛЯ ЛЕТАТЕЛЬНОГО АППАРАТА</article-title><trans-title-group xml:lang="en"><trans-title>AIR CUSHION CHASSIS WITH MULTI-SECTION FORMATION FOR AIRCRAFT</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>Мерзликин</surname><given-names>Ю. Ю.</given-names></name><name name-style="western" xml:lang="en"><surname>Merzlikin</surname><given-names>Y. Y.</given-names></name></name-alternatives><bio xml:lang="ru"><p>главный инженер НИО-12 "Научно-исследовательского Московского комплекса ЦАГИ"</p></bio><email xlink:type="simple">ymerzlikin@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>Долгополов</surname><given-names>А. А.</given-names></name><name name-style="western" xml:lang="en"><surname>Dolgopolov</surname><given-names>A. A.</given-names></name></name-alternatives><bio xml:lang="ru"><p>старший научный сотрудник</p></bio><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>"ФГУП" ЦАГИ</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>168</fpage><lpage>173</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Мерзликин Ю.Ю., Долгополов А.А., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Мерзликин Ю.Ю., Долгополов А.А.</copyright-holder><copyright-holder xml:lang="en">Merzlikin Y.Y., Dolgopolov A.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/268">https://avia.mstuca.ru/jour/article/view/268</self-uri><abstract><p>В данной статье рассматривается разработанное в НИМК ЦАГИ шасси на воздушной подушке (ШВП) с многосекционной ВП, формируемой закрепленными на баллонной части ШВП отдельными эластичными сменными проточными элементами новой конструкции. На установках и в опытовом бассейне НИМК ЦАГИ получены аэрогидродинамические и амортизационные характеристики рассматриваемого ШВП.</p></abstract><trans-abstract xml:lang="en"><p>This article discusses the air cushion chassis with multi-section air cushion, designed in NIMK CAHI. This chassis is formed by separate flexible changeable running elements of an advanced design, which are mounted on the balloon part of an air cushion. Aerohydrodynamic and buffer characteristics of this chassis are achieved through experimental work on the plants and in the experimental pond in NIMK TSAGI.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>летательный аппарат</kwd><kwd>шасси</kwd><kwd>воздушная подушка</kwd><kwd>эксперимент</kwd></kwd-group><kwd-group xml:lang="en"><kwd>aircraft</kwd><kwd>chassis</kwd><kwd>airbag</kwd><kwd>experiment</kwd></kwd-group></article-meta></front><back><ref-list><title>References</title></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>
