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    Experiments and Cohesive Zone Model Parameters for T650/AFR-PE-4/FM680-1 at High Temperatures

    Source: Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 003
    Author:
    Peter A. Gustafson
    ,
    Anthony M. Waas
    DOI: 10.1061/(ASCE)AS.1943-5525.0000083
    Publisher: American Society of Civil Engineers
    Abstract: This 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.
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      Experiments and Cohesive Zone Model Parameters for T650/AFR-PE-4/FM680-1 at High Temperatures

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56226
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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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