Please use this identifier to cite or link to this item: http://hdl.handle.net/20.500.12258/2762
Title: Calculation of the bending of electromechanical aircraft element made of the carbon fiber
Authors: Danilova-Volkovskaya, G. M.
Данилова-Волковская, Г. М.
Begak, A.
Бегак, А.
Keywords: Carbon fibers;Energy management;Motor transportation;Orthotropic plates;Aircraft elements;Method of calculation;Variable thickness;Finite element method
Issue Date: 2017
Publisher: Institute of Physics Publishing
Citation: 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
Series/Report no.: IOP Conference Series: Earth and Environmental Science
Abstract: 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
URI: 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
Appears in Collections:Статьи, проиндексированные в SCOPUS, WOS

Files in This Item:
File Description SizeFormat 
scopusresults 202 .pdf61.7 kBAdobe PDFThumbnail
View/Open
WoS 93 .pdf713.7 kBAdobe PDFThumbnail
View/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.