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Discretization of Thin-Walled Sections with Variable Wall Thickness
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) by a discrete one, consisting of concentrated are...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English Ukrainian |
| Published: |
Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України
2024
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| Online Access: | https://journals.uran.ua/jme/article/view/313042 |
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