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<article 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" xmlns:ali="http://www.niso.org/schemas/ali/1.0/" article-type="research-article" dtd-version="1.2" xml:lang="en"><front><journal-meta><journal-id journal-id-type="publisher-id">Structural Mechanics of Engineering Constructions and Buildings</journal-id><journal-title-group><journal-title xml:lang="en">Structural Mechanics of Engineering Constructions and Buildings</journal-title><trans-title-group xml:lang="ru"><trans-title>Строительная механика инженерных конструкций и сооружений</trans-title></trans-title-group></journal-title-group><issn publication-format="print">1815-5235</issn><issn publication-format="electronic">2587-8700</issn><publisher><publisher-name xml:lang="en">Peoples’ Friendship University of Russia named after Patrice Lumumba (RUDN University)</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="publisher-id">23010</article-id><article-id pub-id-type="doi">10.22363/1815-5235-2020-16-1-54-61</article-id><article-categories><subj-group subj-group-type="toc-heading" xml:lang="en"><subject>Numerical methods of structures’  analysis</subject></subj-group><subj-group subj-group-type="toc-heading" xml:lang="ru"><subject>Численные методы расчета конструкций</subject></subj-group><subj-group subj-group-type="article-type"><subject>Research Article</subject></subj-group></article-categories><title-group><article-title xml:lang="en">Numerical analysis of stability of the stiffened plates subjected aliquant critical loads</article-title><trans-title-group xml:lang="ru"><trans-title>Численный анализ устойчивости подкрепленных пластин с некратными критическими нагрузками</trans-title></trans-title-group></title-group><contrib-group><contrib contrib-type="author"><name-alternatives><name xml:lang="en"><surname>Manuylov</surname><given-names>Gaik A.</given-names></name><name xml:lang="ru"><surname>Мануйлов</surname><given-names>Гайк Александрович</given-names></name></name-alternatives><bio xml:lang="en"><p>Ph.D., Associate Professor</p></bio><bio xml:lang="ru"><p>кандидат технических наук, доцент кафедры cтроительной механики</p></bio><email>kositsyn-s@mail.ru</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><contrib-id contrib-id-type="spin">9390-7610</contrib-id><name-alternatives><name xml:lang="en"><surname>Kositsyn</surname><given-names>Sergey B.</given-names></name><name xml:lang="ru"><surname>Косицын</surname><given-names>Сергей Борисович</given-names></name></name-alternatives><bio xml:lang="en"><p>adviser of the RAACS, D.Sc. in Engineering, Professor of the Department of Theoretical Mechanics</p></bio><bio xml:lang="ru"><p>советник РААСН, доктор технических наук, профессор, заведующий кафедрой теоретической механики</p></bio><email>kositsyn-s@mail.ru</email><xref ref-type="aff" rid="aff1"/></contrib><contrib contrib-type="author"><name-alternatives><name xml:lang="en"><surname>Grudtsyna</surname><given-names>Irina E.</given-names></name><name xml:lang="ru"><surname>Грудцына</surname><given-names>Ирина Евгеньевна</given-names></name></name-alternatives><bio xml:lang="en"><p>postgraduate student of the Department of Theoretical Mechanics</p></bio><bio xml:lang="ru"><p>аспирант кафедры теоретической механики</p></bio><email>kositsyn-s@mail.ru</email><xref ref-type="aff" rid="aff1"/></contrib></contrib-group><aff-alternatives id="aff1"><aff><institution xml:lang="en">Russian University of Transport</institution></aff><aff><institution xml:lang="ru">Российский университет транспорта</institution></aff></aff-alternatives><pub-date date-type="pub" iso-8601-date="2020-12-15" publication-format="electronic"><day>15</day><month>12</month><year>2020</year></pub-date><volume>16</volume><issue>1</issue><issue-title xml:lang="en">VOL 16, NO1 (2020)</issue-title><issue-title xml:lang="ru">ТОМ 16, №1 (2020)</issue-title><fpage>54</fpage><lpage>61</lpage><history><date date-type="received" iso-8601-date="2020-02-27"><day>27</day><month>02</month><year>2020</year></date></history><permissions><copyright-statement xml:lang="en">Copyright ©; 2020, Manuylov G.A., Kositsyn S.B., Grudtsyna I.E.</copyright-statement><copyright-statement xml:lang="ru">Copyright ©; 2020, Мануйлов Г.А., Косицын С.Б., Грудцына И.Е.</copyright-statement><copyright-year>2020</copyright-year><copyright-holder xml:lang="en">Manuylov G.A., Kositsyn S.B., Grudtsyna I.E.</copyright-holder><copyright-holder xml:lang="ru">Мануйлов Г.А., Косицын С.Б., Грудцына И.Е.</copyright-holder><ali:free_to_read xmlns:ali="http://www.niso.org/schemas/ali/1.0/"/><license><ali:license_ref xmlns:ali="http://www.niso.org/schemas/ali/1.0/">http://creativecommons.org/licenses/by/4.0</ali:license_ref></license></permissions><self-uri xlink:href="https://journals.rudn.ru/structural-mechanics/article/view/23010">https://journals.rudn.ru/structural-mechanics/article/view/23010</self-uri><abstract xml:lang="en"><p>The aim of the work is to research the precritical and postcritical equilibrium of the stiffened plates subjected aliquant critical loads. Methods. The finiteelement complex MSC PATRAN - NASTRAN was used in the paper. To simulate the plates, flat four-node elements were used. Calculations taking into account geometric nonlinearity were carried out. The material of the shells was considered absolutely elastic. Results. A technique has been developed to study the stability of reinforced longitudinally compressed plates; the critical forces of the stiffened plates of various thicknesses had been calculated. Graphs of deflections dependences on the value of the compressive load had been constructed. The influence of initial geometric imperfections on the value of the critical loads for stiffened plates has been investigated.</p></abstract><trans-abstract xml:lang="ru"><p>Цели. Исследование докритических и начальных послекритических равновесий подкрепленных продольно сжатых пластин с некратными критическими нагрузками. Методы. Для решения поставленных задач использован конечно-элементный комплекс MSC PATRAN - NASTRAN. Подкрепленные пластины смоделированы плоскими четырехузловыми элементами. Проведены расчеты с учетом геометрической нелинейности. Материал считался абсолютно упругим. Результаты. Разработана методика исследования устойчивости подкрепленных продольно сжатых пластин, определены критические силы подкрепленных пластин различных толщин. Построены графики зависимостей прогибов от величин сжимающих нагрузок. Исследовано влияние начальных геометрических несовершенств на величины критических сил для подкрепленных пластин.</p></trans-abstract><kwd-group xml:lang="ru"><kwd>устойчивость</kwd><kwd>подкрепленная пластина</kwd><kwd>начальные геометрические несовершенства</kwd><kwd>критическая сила</kwd></kwd-group><funding-group/></article-meta></front><body></body><back><ref-list><ref id="B1"><label>1.</label><citation-alternatives><mixed-citation xml:lang="en">Fok W.C., Rhodes J., Walker A.C. Local buckling of outstands in stiffened plates. 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