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: | , , , |
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| Formato: | Статья |
| Idioma: | English |
| Publicado: |
Institute of Physics Publishing
2018
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| Темы: | |
| Acceso en liña: | 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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