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International Journal of Aerospace Engineering
Volume 2018, Article ID 4048386, 13 pages
https://doi.org/10.1155/2018/4048386
Research Article

Application of a Cohesive Zone Model for Simulating Fatigue Crack Growth from Moderate to High Levels of Inconel 718

1School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi’an, China
2State Key Laboratory of Solidification Processing, Northwestern Polytechnical University, Xi’an, China
3School of Aerospace Engineering, Tsinghua University, Beijing, China

Correspondence should be addressed to Huan Li; nc.ude.upwn@nauhil

Received 8 September 2017; Accepted 6 December 2017; Published 1 February 2018

Academic Editor: Roberto G. Citarella

Copyright © 2018 Huan Li et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

How to Cite this Article

Huan Li, Jinshan Li, and Huang Yuan, “Application of a Cohesive Zone Model for Simulating Fatigue Crack Growth from Moderate to High Levels of Inconel 718,” International Journal of Aerospace Engineering, vol. 2018, Article ID 4048386, 13 pages, 2018. https://doi.org/10.1155/2018/4048386.