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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-135</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>Валидация модели заброса птицы на вход в авиационный газотурбинный двигатель</article-title><trans-title-group xml:lang="en"><trans-title>VALIDATION OF AIRCRAFT GAS-TURBINE ENGINE INLET BIRD THROW-IN SIMULATION MODEL</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>Кузьмин</surname><given-names>М. В.</given-names></name><name name-style="western" xml:lang="en"><surname>Kuzmin</surname><given-names>M. V.</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>Кирсанов</surname><given-names>А. Р.</given-names></name><name name-style="western" xml:lang="en"><surname>Kirsanov</surname><given-names>A. R.</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>ОКБ им. А. Люльки</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>120</fpage><lpage>126</lpage><permissions><copyright-statement>Copyright &amp;#x00A9; Кузьмин М.В., Кирсанов А.Р., 2016</copyright-statement><copyright-year>2016</copyright-year><copyright-holder xml:lang="ru">Кузьмин М.В., Кирсанов А.Р.</copyright-holder><copyright-holder xml:lang="en">Kuzmin M.V., Kirsanov A.R.</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/135">https://avia.mstuca.ru/jour/article/view/135</self-uri><abstract><p>Представлено описание процедуры валидации расчетной модели заброса птиц на вход в газотурбинный двигатель (ГТД) и предшествующей верификации ее основных компонентов. Приводятся расчетные и экспериментальные данные в качестве документального свидетельства точности, воспроизводимости и чувствительности модели.</p></abstract><trans-abstract xml:lang="en"><p>This article describes validation procedure of the birds throw into gas-turbine engine (GTE) simulation model and the preceding verification of its main components. The provided data are including predictive and experimental data, as an additional documentary proof of the simulation model fidelity, repeatability and sensitivity.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>валидация модели</kwd><kwd>верификация</kwd><kwd>заброс птиц</kwd><kwd>разрушение</kwd><kwd>газотурбинный авиационный двигатель</kwd></kwd-group><kwd-group xml:lang="en"><kwd>gas-turbine engine</kwd><kwd>birdstrike capacity</kwd><kwd>bird ingestion</kwd><kwd>vulnerability</kwd><kwd>destruction</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">James S. Wilbeck. Impact Behavior of Low Strength Projectiles. Air Force Materials Laboratory. 1977.</mixed-citation><mixed-citation xml:lang="en">James S. Wilbeck. Impact Behavior of Low Strength Projectiles. 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