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pro vyhledávání: '"Mykhailo M. Grebennikov"'
Publikováno v:
Journal of Mechanical Engineering, Vol 27, Iss 3, Pp 34-41 (2024)
At the stage of designing thin-walled aircraft structures, to simplify calculations, their cross sections are idealized. To do this, the section with the skin and the longitudinal elements reinforcing it is replaced (when determining normal stresses)
Externí odkaz:
https://doaj.org/article/a787202bd5d646db863a4bae022f7b0b
