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

Cover Page

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

References

Statistics

Views

Abstract - 153

PDF (Russian) - 94

Cited-By



Copyright (c) 2016 ФИРСАНОВ В.В.

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

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies