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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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