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    Effects of Negative Biaxial Loadings and Notch on Failure Assessment Diagrams

    Source: Journal of Pressure Vessel Technology:;2010:;volume( 132 ):;issue: 001::page 11403
    Author:
    K. Ragupathy
    ,
    D. Hall
    ,
    K. Ramesh
    DOI: 10.1115/1.4000357
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The failure assessment diagram (FAD) is a simplified and robust flaw assessment methodology, which simultaneously connects two dominant failure criteria: linear elastic fracture mechanics on one end and plastic collapse on the other end. This interaction is in the realm of elastic-plastic fracture mechanics. It is popularly known as the R6 approach, which graphically characterizes the impact of plasticity on crack driving force. In recent years, there has been continuous interest in using FADs to assess the failure of cracked structures subjected to biaxial loadings. Biaxiality is defined as the ratio of stress applied parallel and normal to the crack. Some pressure loaded aircraft components operate under negative biaxial ratios up to −0.5. In this paper, a detailed study on FAD was conducted using finite element analysis computed J-integral methods to investigate the effect of biaxial loading using different FAD approaches for geometries with notches. Geometries with a crack that emanates at a fillet region were simulated with various biaxial loading ratios from −0.5 to +0.5 using 2014-T6 material. FAD curves were numerically generated for cracks at notched regions subjected to various biaxial loadings using J-integral values from finite element analyses. These results were compared with standard FAD approaches. All comparison studies were made between uniaxial and biaxial loading cases with FAD curves created using four different crack sizes. Under small scale yielding, this study clearly shows that FAD curves are not influenced by negative biaxial loading at low load (up to 40% of yield strength). It was clearly confirmed that the majority of previously developed analytical FAD curves do not effectively account for notch and plasticity effects due to negative biaxiality. Based on this study, tension normal to the crack and compression parallel to the crack is the worst combination, and it has a very pronounced effect on FAD curve shapes. The standard analytical FAD curves are nonconservative compared with the approach recommended here, particularly under the worst case condition. FAD curves developed are shown to predict lower failure loads as compared with the currently accepted analytical FAD approaches defined in existing standards, e.g., R6 and API 579. The impact of negative biaxial loading can be investigated directly using a J-integral FAD approach but can be compared with ease by plotting both approaches in a FAD format.
    keyword(s): Stress , Fracture (Materials) , Finite element analysis , Stress , Failure , Yield strength , Equations , Force AND Plasticity ,
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      Effects of Negative Biaxial Loadings and Notch on Failure Assessment Diagrams

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    https://yetl.yabesh.ir/yetl1/handle/yetl/144725
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    contributor authorK. Ragupathy
    contributor authorD. Hall
    contributor authorK. Ramesh
    date accessioned2017-05-09T00:40:39Z
    date available2017-05-09T00:40:39Z
    date copyrightFebruary, 2010
    date issued2010
    identifier issn0094-9930
    identifier otherJPVTAS-28525#011403_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/144725
    description abstractThe failure assessment diagram (FAD) is a simplified and robust flaw assessment methodology, which simultaneously connects two dominant failure criteria: linear elastic fracture mechanics on one end and plastic collapse on the other end. This interaction is in the realm of elastic-plastic fracture mechanics. It is popularly known as the R6 approach, which graphically characterizes the impact of plasticity on crack driving force. In recent years, there has been continuous interest in using FADs to assess the failure of cracked structures subjected to biaxial loadings. Biaxiality is defined as the ratio of stress applied parallel and normal to the crack. Some pressure loaded aircraft components operate under negative biaxial ratios up to −0.5. In this paper, a detailed study on FAD was conducted using finite element analysis computed J-integral methods to investigate the effect of biaxial loading using different FAD approaches for geometries with notches. Geometries with a crack that emanates at a fillet region were simulated with various biaxial loading ratios from −0.5 to +0.5 using 2014-T6 material. FAD curves were numerically generated for cracks at notched regions subjected to various biaxial loadings using J-integral values from finite element analyses. These results were compared with standard FAD approaches. All comparison studies were made between uniaxial and biaxial loading cases with FAD curves created using four different crack sizes. Under small scale yielding, this study clearly shows that FAD curves are not influenced by negative biaxial loading at low load (up to 40% of yield strength). It was clearly confirmed that the majority of previously developed analytical FAD curves do not effectively account for notch and plasticity effects due to negative biaxiality. Based on this study, tension normal to the crack and compression parallel to the crack is the worst combination, and it has a very pronounced effect on FAD curve shapes. The standard analytical FAD curves are nonconservative compared with the approach recommended here, particularly under the worst case condition. FAD curves developed are shown to predict lower failure loads as compared with the currently accepted analytical FAD approaches defined in existing standards, e.g., R6 and API 579. The impact of negative biaxial loading can be investigated directly using a J-integral FAD approach but can be compared with ease by plotting both approaches in a FAD format.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Negative Biaxial Loadings and Notch on Failure Assessment Diagrams
    typeJournal Paper
    journal volume132
    journal issue1
    journal titleJournal of Pressure Vessel Technology
    identifier doi10.1115/1.4000357
    journal fristpage11403
    identifier eissn1528-8978
    keywordsStress
    keywordsFracture (Materials)
    keywordsFinite element analysis
    keywordsStress
    keywordsFailure
    keywordsYield strength
    keywordsEquations
    keywordsForce AND Plasticity
    treeJournal of Pressure Vessel Technology:;2010:;volume( 132 ):;issue: 001
    contenttypeFulltext
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