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contributor authorPeter A. Gustafson
contributor authorAnthony M. Waas
date accessioned2017-05-08T21:33:47Z
date available2017-05-08T21:33:47Z
date copyrightJuly 2011
date issued2011
identifier other%28asce%29as%2E1943-5525%2E0000083.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56226
description abstractThis paper reports an experimental program to establish a cohesive zone model for the T650/AFR-PE-4 (laminate) and FM680-1 (adhesive) system. The cohesive zone model is based on a four parameter characterization: in each mode, a range of values for the critical energy release rate and cohesive strength are computed from a set of experimental results. Values of each parameter are determined over the temperature range of 20–350°C. Owing to experimental limitations, two methods for determining the Mode I critical energy release rate are reported from the double cantilever beam test: the area method and the inverse method. The Mode I strength is determined from a button peel stress test. The values of the Mode II parameters are determined by using a mapping procedure that accounts for multiparameter dependence in models of the end notch flexure and single lap joint tests.
publisherAmerican Society of Civil Engineers
titleExperiments and Cohesive Zone Model Parameters for T650/AFR-PE-4/FM680-1 at High Temperatures
typeJournal Paper
journal volume24
journal issue3
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000083
treeJournal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003
contenttypeFulltext


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