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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Главные авторы:	Danilova-Volkovskaya, G., Данилова-Волковская, Г., Begak, A., Бегак, А.
格式:	Статья
语言:	English
出版:	Institute of Physics Publishing 2018
主题:	Carbon fibers Energy management Motor transportation Orthotropic plates Aircraft elements Method of calculation Variable thickness Finite element method
在线阅读:	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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Calculation of the bending of electromechanical aircraft element made of the carbon fiber

由 Danilova-Volkovskaya, G. M., Данилова-Волковская, Г. М., Begak, A., Бегак, А.
出版 2018

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

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