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contributor authorJohn D. Pratt
contributor authorGerard Pardoen
date accessioned2017-05-08T21:16:05Z
date available2017-05-08T21:16:05Z
date copyrightJanuary 2002
date issued2002
identifier other%28asce%290893-1321%282002%2915%3A1%2820%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44957
description abstractNonlinear finite-element models are developed that predict the load-elongation behavior of conical-head bolted lap joints, and the load-elongation predictions are compared with experimental test data. The study is conducted for several panel thicknesses with three fastener sizes and three panel materials. The model load-elongation predictions are in excellent agreement with experimental test data. Model parameters, such as part discretization, material model selection, sliding interface friction coefficients, and convergence tolerances, are discussed. A means of inducing clamp in the joint is also developed. The results show that nonlinear finite-element analysis may reliably predict the behavior of conical-head bolted joints.
publisherAmerican Society of Civil Engineers
titleNumerical Modeling of Bolted Lap Joint Behavior
typeJournal Paper
journal volume15
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2002)15:1(20)
treeJournal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 001
contenttypeFulltext


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