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Numerical analysis on initial cracking load of wing crack based on extended finite element method
发表时间:2019-03-11 点击次数:
论文类型:期刊论文
第一作者:Yang Q.
通讯作者:Yang, Q.; School of Civil and Hydraulic Engineering, State Key Lab. of Coastal and Offshore engineering, Dalian University of Technology, Dalian, China; email: qyang@dlut.edu.cn
合写作者:Wang C.
发表时间:2010-01-01
发表刊物:Electronic Journal of Geotechnical Engineering
收录刊物:EI、Scopus
文献类型:J
卷号:15 O
页面范围:1641-1646
ISSN号:10893032
摘要:All the experiments on the mixed mode fractures in quasi-rock materials under compression-shear loading showed that the initial cracking load of wing crack is related to the angle of flaw, but how it works, many scholars can't obtain consistency. A numerical analysis based on extended finite element method has been carried out, the propagation progress of wind crack has been simulated, the reasons of inconsistency were obtained by the load-displacement curve. The numerical results shows: (1) The initial cracking load of wing crack increase as the increasing of flaw angle, the propagation load of wing cracks with larger flaw angle are larger than that with smaller ones when wing cracks reach a certain length; (2) The displacement is small at the beginning of the propagation of wing crack, so the increment step should be suitable. The research achievements show a good explanation to the contradiction and also have theory instruction function to the relevant experiments in the future. ? 2008 ejge.
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