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dc.contributor.authorDanilova-Volkovskaya, G. M.-
dc.contributor.authorДанилова-Волковская, Г. М.-
dc.contributor.authorBegak, A.-
dc.contributor.authorБегак, А.-
dc.date.accessioned2018-08-03T10:00:47Z-
dc.date.available2018-08-03T10:00:47Z-
dc.date.issued2017-
dc.identifier.citationDanilova-Volkovskaya, G., Chepurnenko, A., Begak, A., Savchenko, A. Calculation of the bending of electromechanical aircraft element made of the carbon fiber // IOP Conference Series: Earth and Environmental Science. - 2017. - Volume 90. - Issue 1. - Номер статьи 012046ru
dc.identifier.urihttps://www.scopus.com/record/display.uri?eid=2-s2.0-85035068613&origin=resultslist&sort=plf-f&src=s&nlo=1&nlr=20&nls=afprfnm-t&affilName=North+Caucasus+Federal+University&sid=9495f4ffec2abf1c12b163540c53172c&sot=afnl&sdt=sisr&sl=53&s=%28AF-ID%28%22North+Caucasus+Federal+University%22+60070541%29%29&ref=%28Calculation+of+the+bending+of+electromechanical+aircraft+element+made+of+the+carbon+fiber%29&relpos=0&citeCnt=0&searchTerm=-
dc.identifier.urihttp://hdl.handle.net/20.500.12258/2762-
dc.description.abstractWe consider a method of calculation of an orthotropic plate with variable thickness. The solution is performed numerically by the finite element method. The calculation is made for the springs of a hang glider made of carbon fiber. The comparison of the results with Sofistik software complex is givenru
dc.language.isoenru
dc.publisherInstitute of Physics Publishingru
dc.relation.ispartofseriesIOP Conference Series: Earth and Environmental Science-
dc.subjectCarbon fibersru
dc.subjectEnergy managementru
dc.subjectMotor transportationru
dc.subjectOrthotropic platesru
dc.subjectAircraft elementsru
dc.subjectMethod of calculationru
dc.subjectVariable thicknessru
dc.subjectFinite element methodru
dc.titleCalculation of the bending of electromechanical aircraft element made of the carbon fiberru
dc.typeСтатьяru
vkr.instИнститут сервиса, туризма и дизайна (филиал) СКФУ в г. Пятигорске-
Appears in Collections:Статьи, проиндексированные в SCOPUS, WOS

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