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    Fracture Toughness of 7075-T6 and -T651 Sheet, Plate, and Multilayered Adhesive-Bonded Panels

    Source: Journal of Fluids Engineering:;1967:;volume( 089 ):;issue: 003::page 503
    Author:
    J. G. Kaufman
    DOI: 10.1115/1.3609649
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fracture-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.
    keyword(s): Adhesives , Fracture toughness , Thickness , Fracture (Process) , Stress , Shear (Mechanics) , Plane strain AND Package on package ,
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      Fracture Toughness of 7075-T6 and -T651 Sheet, Plate, and Multilayered Adhesive-Bonded Panels

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/119689
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    • Journal of Fluids Engineering

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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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