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contributor authorJohn D. Pratt
contributor authorGerard Pardoen
date accessioned2017-05-08T21:16:06Z
date available2017-05-08T21:16:06Z
date copyrightApril 2002
date issued2002
identifier other%28asce%290893-1321%282002%2915%3A2%2855%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44961
description abstractNonlinear finite-element models that predict the load-elongation behavior of single- and dual-bolted conical-head bolted lap joints are developed, and the load-elongation predictions are compared with experimental test data. The study is conducted for several panel thicknesses with a 4.8 mm size fastener and 2024-T3 clad aluminum alloy panels. The model load-elongation predictions are in excellent agreement with experimental test data. The results show that (1) dual-bolted lap joint test results underpredict the strength of single-bolted lap joints; and (2) numerical models may reliably predict the load-elongation behavior of mechanically fastened lap joints at a fraction of the cost and time of experimental testing.
publisherAmerican Society of Civil Engineers
titleComparative Behavior of Single-Bolted and Dual-Bolted Lap Joints
typeJournal Paper
journal volume15
journal issue2
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2002)15:2(55)
treeJournal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 002
contenttypeFulltext


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