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    Curvilinear Fatigue Crack Growth Simulation and Validation under Constant Amplitude and Overload Loadings

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 001
    Author:
    Zizi Lu
    ,
    Jifeng Xu
    ,
    Lei Wang
    ,
    Jianren Zhang
    ,
    Yongming Liu
    DOI: 10.1061/(ASCE)AS.1943-5525.0000337
    Publisher: American Society of Civil Engineers
    Abstract: A concurrent simulation and experimental validation for curvilinear fatigue crack growth (FCG) analysis under both constant amplitude and overload spectrums is proposed in this paper. The simulation methodology is based on a small time-scale fatigue crack growth model and the extended finite element method (XFEM) to calculate the stress intensity factor solution of an arbitrary curvilinear crack. Parametric studies are used to determine the algorithm parameters in the numerical fatigue crack growth simulation. Following this, experimental testing on modified compact specimens is performed under both constant amplitude and overload loadings for model validation. Experimentally measured crack growth orientations and lengths are compared with numerical simulations. Both the experimental and simulation results show the overload retardation behavior for curvilinear cracks under overload loadings. The investigated periodic overload loading has no significant impact on the crack growth orientations. Several conclusions and areas of future work are identified based on the proposed numerical and experimental investigations.
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      Curvilinear Fatigue Crack Growth Simulation and Validation under Constant Amplitude and Overload Loadings

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    http://yetl.yabesh.ir/yetl1/handle/yetl/56485
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    contributor authorZizi Lu
    contributor authorJifeng Xu
    contributor authorLei Wang
    contributor authorJianren Zhang
    contributor authorYongming Liu
    date accessioned2017-05-08T21:34:25Z
    date available2017-05-08T21:34:25Z
    date copyrightJanuary 2015
    date issued2015
    identifier other%28asce%29as%2E1943-5525%2E0000340.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56485
    description abstractA concurrent simulation and experimental validation for curvilinear fatigue crack growth (FCG) analysis under both constant amplitude and overload spectrums is proposed in this paper. The simulation methodology is based on a small time-scale fatigue crack growth model and the extended finite element method (XFEM) to calculate the stress intensity factor solution of an arbitrary curvilinear crack. Parametric studies are used to determine the algorithm parameters in the numerical fatigue crack growth simulation. Following this, experimental testing on modified compact specimens is performed under both constant amplitude and overload loadings for model validation. Experimentally measured crack growth orientations and lengths are compared with numerical simulations. Both the experimental and simulation results show the overload retardation behavior for curvilinear cracks under overload loadings. The investigated periodic overload loading has no significant impact on the crack growth orientations. Several conclusions and areas of future work are identified based on the proposed numerical and experimental investigations.
    publisherAmerican Society of Civil Engineers
    titleCurvilinear Fatigue Crack Growth Simulation and Validation under Constant Amplitude and Overload Loadings
    typeJournal Paper
    journal volume28
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000337
    treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 001
    contenttypeFulltext
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