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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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