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    Effects of Interleaves on Fracture of Laminated Composites: Part II—Solution and Results

    Source: Journal of Applied Mechanics:;1990:;volume( 057 ):;issue: 001::page 175
    Author:
    A. K. Kaw
    ,
    J. G. Goree
    DOI: 10.1115/1.2888299
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The numerical solution of the integral equations derived in Part I of this work is developed and the critical stresses and displacements are calculated. These results indicate that interleaves increase the interfacial damage tolerance and significantly relieve the stresses in the undamaged plies. Interface (H-shaped) cracks have a stable growth with the mode I opening stress becoming compressive after a small longitudinal growth. Additional interface crack extension is due to shear stresses (mode II) only. In order to recommend an interleaf thickness-to-layer width ratio, the influence of relative material properties, structural weight, and stress reduction is studied.
    keyword(s): Composite materials , Fracture (Process) , Stress , Fracture (Materials) , Materials properties , Shear (Mechanics) , Integral equations , Thickness AND Weight (Mass) ,
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      Effects of Interleaves on Fracture of Laminated Composites: Part II—Solution and Results

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/106525
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    contributor authorA. K. Kaw
    contributor authorJ. G. Goree
    date accessioned2017-05-08T23:31:58Z
    date available2017-05-08T23:31:58Z
    date copyrightMarch, 1990
    date issued1990
    identifier issn0021-8936
    identifier otherJAMCAV-26318#175_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106525
    description abstractThe numerical solution of the integral equations derived in Part I of this work is developed and the critical stresses and displacements are calculated. These results indicate that interleaves increase the interfacial damage tolerance and significantly relieve the stresses in the undamaged plies. Interface (H-shaped) cracks have a stable growth with the mode I opening stress becoming compressive after a small longitudinal growth. Additional interface crack extension is due to shear stresses (mode II) only. In order to recommend an interleaf thickness-to-layer width ratio, the influence of relative material properties, structural weight, and stress reduction is studied.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Interleaves on Fracture of Laminated Composites: Part II—Solution and Results
    typeJournal Paper
    journal volume57
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2888299
    journal fristpage175
    journal lastpage181
    identifier eissn1528-9036
    keywordsComposite materials
    keywordsFracture (Process)
    keywordsStress
    keywordsFracture (Materials)
    keywordsMaterials properties
    keywordsShear (Mechanics)
    keywordsIntegral equations
    keywordsThickness AND Weight (Mass)
    treeJournal of Applied Mechanics:;1990:;volume( 057 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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