STRESS STATE CALLED AS "BOUNDARY LAYER" IS BOUNDARY TORSION OF THE RECTANGULAR PLATE
- Authors: Firsanov V.V1
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Affiliations:
- Moskovskiy Aviazionniy Institute, Moscow, Russia
- Issue: No 6 (2016)
- Pages: 44-51
- Section: Articles
- URL: https://journal-vniispk.ru/1815-5235/article/view/346435
- ID: 346435
Cite item
Abstract
Boundary value problem formulated for determining stress state of type "boundary layer" is identically to torsion deformation of edges, and its solution in a way bring to the Dirichlet's problem is given. As a result of calculations, the essential contribution of the boundary torsion stress-strain state to the general stress-strain state of a plate is shown, that is very important for the estimation of strength for various units in thin-walled elements of aircraft structures.
About the authors
Val V Firsanov
Moskovskiy Aviazionniy Institute, Moscow, Russia
Email: k906@mai.ru
д-р техн. наук, профессор 125993 Москва, А-80, ГСП-3, Волоколамское шоссе, д.4
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