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contributor authorJ. G. Kaufman
date accessioned2017-05-08T23:55:16Z
date available2017-05-08T23:55:16Z
date copyrightSeptember, 1967
date issued1967
identifier issn0098-2202
identifier otherJFEGA4-27300#503_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119689
description abstractFracture-toughness tests have been made of 7075-T6 sheet and -T651 plate and of multi-layered panels of the sheet and plate. The nominal net fracture strength and the critical fracture-toughness parameters (Kc and Gc ) of multilayered adhesive-bonded panels are greater than those of sheet or plate of the same total thickness, because the individual layers may fracture independently, each developing shear surfaces. The fracture strength and critical stress intensity factor, Kc , for a 0.5-in. thick panel made up of eight layers of 0.063-in. sheet are approximately twice those of 0.5-in. plate. Multilayered metallurgically bonded panels do not exhibit any advantage over sheet or plate of the same thickness, if the metallurgical bond retards shear-surface formation on the individual layers. The plane-strain stress-intensity factor, determined at pop-in on multi-layered adhesive-bonded or metallurgically bonded panels, is independent of thickness or number of layers.
publisherThe American Society of Mechanical Engineers (ASME)
titleFracture Toughness of 7075-T6 and -T651 Sheet, Plate, and Multilayered Adhesive-Bonded Panels
typeJournal Paper
journal volume89
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3609649
journal fristpage503
journal lastpage507
identifier eissn1528-901X
keywordsAdhesives
keywordsFracture toughness
keywordsThickness
keywordsFracture (Process)
keywordsStress
keywordsShear (Mechanics)
keywordsPlane strain AND Package on package
treeJournal of Fluids Engineering:;1967:;volume( 089 ):;issue: 003
contenttypeFulltext


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