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    Adhesive Bond Stresses and Strains at Discontinuities and Cracks in Bonded Structures

    Source: Journal of Engineering Materials and Technology:;1978:;volume( 100 ):;issue: 001::page 16
    Author:
    L. J. Hart-Smith
    DOI: 10.1115/1.3443442
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents analysis procedures to be used for analyzing adhesively bonded structures containing cracks or discontinuities in the metal elements. The analyses are performed for a range of disbonds in each of four basic problems for stiffened structures: (1) stiffener broken at one station or with a finite length removed, sheet intact, (2) stiffener intact, sheet completely broken, (3) one-bay sheet crack, stiffeners intact, and (4) two-bay sheet crack, stiffener intact. Separate failure modes of disbond under shear loads, stiffener yield, and sheet fast fracture are investigated. The solutions are essentially planar (two-dimensional) and such three-dimensional effects as stiffener or sheet bending and peel stresses in the adhesives are not accounted for. The paper contains parametric studies for the governing variables and excellent agreement with test is demonstrated for the available test data (one-bay sheet crack). The analyses are approximate and not of universal applicability, but are simple to use with either pocket electronic calculators or digital computers. Known limitations of the theory are confined to situations in which the adhesive stresses are small and widespread rather than high and concentrated in a small identifiable zone adjacent to the discontinuity. The conconclusion drawn from the examples investigated is that disbonds can be initiated relatively easily at discontinuities in the metal structural elements, because the bond is very stiff, and that care is needed in proportioning the structural elements to control this potential problem. The analyses indicate also that the initial disbond is usually self-arresting and is not catastrophic. Higher loads are usually needed to propagate the disbond and, eventually, induce complete failure which is triggered by stiffener yield or fast fracture of the sheet at the crack tips. The sample cases point to the need to account for adhesive plasticity, stiffener yielding, and changes in load path as disbonds propagate.
    keyword(s): Adhesives , Stress , Fracture (Materials) , Fracture (Process) , Structural elements (Construction) , Metals , Failure , Plasticity , Computers AND Shear (Mechanics) ,
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      Adhesive Bond Stresses and Strains at Discontinuities and Cracks in Bonded Structures

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    https://yetl.yabesh.ir/yetl1/handle/yetl/91110
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    contributor authorL. J. Hart-Smith
    date accessioned2017-05-08T23:04:56Z
    date available2017-05-08T23:04:56Z
    date copyrightJanuary, 1978
    date issued1978
    identifier issn0094-4289
    identifier otherJEMTA8-26859#16_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91110
    description abstractThis paper presents analysis procedures to be used for analyzing adhesively bonded structures containing cracks or discontinuities in the metal elements. The analyses are performed for a range of disbonds in each of four basic problems for stiffened structures: (1) stiffener broken at one station or with a finite length removed, sheet intact, (2) stiffener intact, sheet completely broken, (3) one-bay sheet crack, stiffeners intact, and (4) two-bay sheet crack, stiffener intact. Separate failure modes of disbond under shear loads, stiffener yield, and sheet fast fracture are investigated. The solutions are essentially planar (two-dimensional) and such three-dimensional effects as stiffener or sheet bending and peel stresses in the adhesives are not accounted for. The paper contains parametric studies for the governing variables and excellent agreement with test is demonstrated for the available test data (one-bay sheet crack). The analyses are approximate and not of universal applicability, but are simple to use with either pocket electronic calculators or digital computers. Known limitations of the theory are confined to situations in which the adhesive stresses are small and widespread rather than high and concentrated in a small identifiable zone adjacent to the discontinuity. The conconclusion drawn from the examples investigated is that disbonds can be initiated relatively easily at discontinuities in the metal structural elements, because the bond is very stiff, and that care is needed in proportioning the structural elements to control this potential problem. The analyses indicate also that the initial disbond is usually self-arresting and is not catastrophic. Higher loads are usually needed to propagate the disbond and, eventually, induce complete failure which is triggered by stiffener yield or fast fracture of the sheet at the crack tips. The sample cases point to the need to account for adhesive plasticity, stiffener yielding, and changes in load path as disbonds propagate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAdhesive Bond Stresses and Strains at Discontinuities and Cracks in Bonded Structures
    typeJournal Paper
    journal volume100
    journal issue1
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.3443442
    journal fristpage16
    journal lastpage24
    identifier eissn1528-8889
    keywordsAdhesives
    keywordsStress
    keywordsFracture (Materials)
    keywordsFracture (Process)
    keywordsStructural elements (Construction)
    keywordsMetals
    keywordsFailure
    keywordsPlasticity
    keywordsComputers AND Shear (Mechanics)
    treeJournal of Engineering Materials and Technology:;1978:;volume( 100 ):;issue: 001
    contenttypeFulltext
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