STRESS STATE CALLED AS "BOUNDARY LAYER" IS BOUNDARY TORSION OF THE RECTANGULAR PLATE
- Authors: Firsanov V.V1
-
Affiliations:
- Moskovskiy Aviazionniy Institute, Moscow, Russia
- Issue: No 6 (2016)
- Pages: 44-51
- Section: Articles
- URL: https://journals.rudn.ru/structural-mechanics/article/view/14619
Cite item
Full Text
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