STRESS STATE CALLED AS "BOUNDARY LAYER" IS BOUNDARY TORSION OF THE RECTANGULAR PLATE: Fid-Bau Portal

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

Val V Firsanov

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.

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

Val V Firsanov

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.

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

Val V Firsanov

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.

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Title:

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

Contributors:

Val V Firsanov (author)

Published in:

Structural Mechanics of Engineering Constructions and Buildings, Vol 0, Iss 6, Pp 44-51 (2016)

Publication date:

2016

ISSN:

1815-5235 , 2587-8700

Type of media:

Article (Journal)

Type of material:

Electronic Resource

Language:

Unknown

Keywords:

прямоугольная пластинка , трехмерные уравнения теории упругости , метод прямого асимптотического интегрирования , краевые задачи , основное напряженно-деформированное состояние , напряженное состояние «пограничный слой» , быстро затухающее напряженное состояние кручения закрепленного края пластинки , задача Дирихле , Architectural engineering. Structural engineering of buildings , TH845-895

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