Calculation of the bending of electromechanical aircraft element made of the carbon fiber

We 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 give...

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Päätekijät:	Danilova-Volkovskaya, G., Данилова-Волковская, Г., Begak, A., Бегак, А.
Aineistotyyppi:	Статья
Kieli:	English
Julkaistu:	Institute of Physics Publishing 2018
Aiheet:	Carbon fibers Energy management Motor transportation Orthotropic plates Aircraft elements Method of calculation Variable thickness Finite element method
Linkit:	https://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= https://dspace.ncfu.ru/handle/20.500.12258/2762
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spelling	oai:10.200.131.19:20.500.12258-27622018-08-03T10:01:21Z Calculation of the bending of electromechanical aircraft element made of the carbon fiber Danilova-Volkovskaya, G. Данилова-Волковская, Г. Begak, A. Бегак, А. Carbon fibers Energy management Motor transportation Orthotropic plates Aircraft elements Method of calculation Variable thickness Finite element method We 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 given 2018-08-03T10:00:47Z 2018-08-03T10:00:47Z 2017 Статья Danilova-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 012046 https://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= http://hdl.handle.net/20.500.12258/2762 en IOP Conference Series: Earth and Environmental Science application/pdf application/pdf Institute of Physics Publishing
institution	СКФУ
collection	Репозиторий
language	English
topic	Carbon fibers Energy management Motor transportation Orthotropic plates Aircraft elements Method of calculation Variable thickness Finite element method
spellingShingle	Carbon fibers Energy management Motor transportation Orthotropic plates Aircraft elements Method of calculation Variable thickness Finite element method Danilova-Volkovskaya, G. Данилова-Волковская, Г. Begak, A. Бегак, А. Calculation of the bending of electromechanical aircraft element made of the carbon fiber
description	We 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 given
format	Статья
author	Danilova-Volkovskaya, G. Данилова-Волковская, Г. Begak, A. Бегак, А.
author_facet	Danilova-Volkovskaya, G. Данилова-Волковская, Г. Begak, A. Бегак, А.
author_sort	Danilova-Volkovskaya, G.
title	Calculation of the bending of electromechanical aircraft element made of the carbon fiber
title_short	Calculation of the bending of electromechanical aircraft element made of the carbon fiber
title_full	Calculation of the bending of electromechanical aircraft element made of the carbon fiber
title_fullStr	Calculation of the bending of electromechanical aircraft element made of the carbon fiber
title_full_unstemmed	Calculation of the bending of electromechanical aircraft element made of the carbon fiber
title_sort	calculation of the bending of electromechanical aircraft element made of the carbon fiber
publisher	Institute of Physics Publishing
publishDate	2018
url	https://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= https://dspace.ncfu.ru/handle/20.500.12258/2762
work_keys_str_mv	AT danilovavolkovskayag calculationofthebendingofelectromechanicalaircraftelementmadeofthecarbonfiber AT danilovavolkovskaâg calculationofthebendingofelectromechanicalaircraftelementmadeofthecarbonfiber AT begaka calculationofthebendingofelectromechanicalaircraftelementmadeofthecarbonfiber AT begaka calculationofthebendingofelectromechanicalaircraftelementmadeofthecarbonfiber
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Calculation of the bending of electromechanical aircraft element made of the carbon fiber

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