STRESS STATE CALLED AS "BOUNDARY LAYER" IS BOUNDARY TORSION OF THE RECTANGULAR PLATE

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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

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Copyright (c) 2016 ФИРСАНОВ В.В.

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This work is licensed under a Creative Commons Attribution 4.0 International License.

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