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contributor authorJohn D. Pratt
contributor authorGerard Pardoen
date accessioned2017-05-08T21:16:07Z
date available2017-05-08T21:16:07Z
date copyrightOctober 2002
date issued2002
identifier other%28asce%290893-1321%282002%2915%3A4%28136%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44971
description abstractNumerical models of single-fastener bolted lap joints are developed in which the effect of the head angle and height on joint elongation are studied for three fastener sizes, three panel materials, and several panel thicknesses. Baseline 100° bolt-head angle numerical models are calibrated and validated with experimental data. These baseline models are then modified to predict the load-elongation behavior of lap joints with five different head angles and four different head heights. The numerical predictions are summarized in graphical form. The results show that the fastener head height has a much greater influence on joint-slip resistance than does the angle, with the shallower heads providing the greatest resistance to joint elongation under load.
publisherAmerican Society of Civil Engineers
titleInfluence of Head Geometry on Bolted Joint Behavior
typeJournal Paper
journal volume15
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2002)15:4(136)
treeJournal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 004
contenttypeFulltext


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