Open Access
Issue
JNWPU
Volume 37, Number 4, August 2019
Page(s) 737 - 743
DOI https://doi.org/10.1051/jnwpu/20193740737
Published online 23 September 2019
  1. Federal Aviation Administration. Damage Tolerance and Fatigue Evaluation of Structure[S]. AC 25.571-1D, 2011 [Google Scholar]
  2. Belytschko T, Black T. Elastic Crack Growth in Finite Elements with Minimal Remeshing[J]. International Journal for Numerical Methods in Engineering, 1999, 86: 1141–1151 [Google Scholar]
  3. Moes N, Dolbow J, Belytschko T. A Finite Element Method for Crack Growth without Remeshing[J]. International Journal for Numerical Methods in Engineering, 2015, 46: 131–150[Article] [NASA ADS] [CrossRef] [Google Scholar]
  4. Bergara A, Dorado J I, Martin-Meizoro A, et al. Fatigue Crack Propagation in Complex Stress Fields:Experiments and Numerical Simulations Using the Extended Finite Element Method(XFEM)[J]. International Journal of Fatigue, 2017, 103: 112–121 [Article] [CrossRef] [Google Scholar]
  5. Dirik H, Yalcinkaya T. Crack Path and Life Prediction under Mixed Mode Cycle Variable Amplitude Loading through XFEM[J]. International Journal of Fatigue, 2018, 114: 34–50 [Article] [CrossRef] [Google Scholar]
  6. Menk A B, Ttephane Pierre Alain. Crack Growth Calculations in Solder Joints Based on Microstructural Phenomena with X-FEM[J]. Computational Material Science, 2011, 50(3): 1145–1156 [Article] [CrossRef] [Google Scholar]
  7. Wang Chong, Lu Tongli. Analysis of Crack Growth at Countersink Hole of Airplane Skinbased on FEM[J]. Journal of Shanghai University of Engineering Science, 2011, 25(2): 117–120 [Article] (In chinese) [Google Scholar]
  8. Su Yi, Wang Shengnan. Analysis of Fatigue and Damage Tolerance of Joint Region of Aircraft Certain Part[J]. Aeronautical Computing Technique, 2013, 43(3): 45–47 [Article] (In chinese) [NASA ADS] [Google Scholar]
  9. Lu Yongjun, Zhang Huanqing, Wang Fenghui, et al. Applicaton of Extended Finite Element Method in Fatigue Life Estimation of Structural Components[J]. Chinese Journal of Applied Mechanics Echanics, 2016, 33(3): 441–446 [Article] (In chinese) [Google Scholar]
  10. Forth S C, Wright C W, Johnston W M. 7075-T6 and 2024-T351 Aluminum Alloy Fatigue Crack Growth Rate Data[R]. NASA/TM-2005-213907, 2005 [Google Scholar]

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