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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#733_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123206
description abstractThis paper treats the effective antiplane shear response of a composite consisting of fibers that interact with the matrix through nonlinear Needleman-type cohesive zones. The first paper (Part I) examines effective axial tension response. The composite cylinders representation of a representative volume element (RVE) is employed throughout. For antiplane shear loading the elastic field solution for a single composite cylinder is found in the form of a series expansion whose coefficients are governed by an infinite set of nonlinear equations. Bounds on the total potential energy and the total complementary energy of an RVE do not coincide although they are shown to differ by a term of order O(c4) where c is the fiber volume concentration. Interaction effects due to finite volume concentration, coupled with nonlinear interface characterization, are shown to precipitate instability in composite response. [S0021-8936(00)02104-8]
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Fiber Composite With Nonlinear Interface—Part II: Antiplane Shear
typeJournal Paper
journal volume67
journal issue4
journal titleJournal of Applied Mechanics
identifier doi10.1115/1.1329320
journal fristpage733
journal lastpage739
identifier eissn1528-9036
keywordsShear (Mechanics)
keywordsBoundary-value problems
keywordsCylinders
keywordsDisplacement
keywordsComposite materials
keywordsFibers
keywordsTraction AND Stress
treeJournal of Applied Mechanics:;2000:;volume( 067 ):;issue: 004
contenttypeFulltext


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