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contributor authorA. J. Levy
date accessioned2017-05-09T00:01:38Z
date available2017-05-09T00:01:38Z
date copyrightDecember, 2000
date issued2000
identifier issn0021-8936
identifier otherJAMCAV-26501#727_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123205
description abstractThis paper treats the effective axial tension response of a composite consisting of fibers that debond from the matrix according to nonlinear Needleman-type cohesive zones. A second, related paper (Part II) treats effective antiplane shear response. The composite cylinders representation of a representative volume element (RVE) is employed throughout. For axial tension loading a simple rotationally symmetric boundary value problem for a single composite cylinder is solved. Bounds on the total potential energy and the total complementary energy are shown to coincide and an exact solution for axial extension and Poisson contraction of an RVE of the composite is obtained. Nonlinear interfacial debonding, however, is shown to have a negligible effect on extensional response and only a small, though potentially destabilizing, effect on Poisson contraction response. [S0021-8936(00)02004-3]
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Fiber Composite With Nonlinear Interface—Part I: Axial Tension
typeJournal Paper
journal volume67
journal issue4
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.1329319
journal fristpage727
journal lastpage732
identifier eissn1528-9036
keywordsComposite materials
keywordsFibers
keywordsCylinders
keywordsTension AND Force
treeJournal of Applied Mechanics:;2000:;volume( 067 ):;issue: 004
contenttypeFulltext


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