Prediction of Crack Initiation Site in Fastener Hole of Composite Laminate-Reference-Cited by-同舟云学术

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Prediction of Crack Initiation Site in Fastener Hole of Composite Laminate

Published:2015-02-20 Issue: Volume: Page:185-198
ISSN:
Container-title:Advanced Composites for Aerospace, Marine, and Land Applications II
language:
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Author:

Sallam Hossam El-Din M.,Abd-Elhady Amr A.

Publisher

John Wiley & Sons, Inc.

Reference15 articles.

1. Failure Load Prediction of Mechanically Fastened Composite Joints;Choi;Journal of Composite Materials,2003

2. Progressive Failure Analysis of Bolted Single-Lap Composite Joint Based on Extended Finite Element Method;Wang;Materials and Design,2012

3. G. M. K. Pearce A. F. Johnson A. K. Hellier R. S. Thomson “A Stacked-Shell Finite Element Approach for Modeling a Dynamically Loaded Composite Bolted Joint Under in- Plane Bearing Loads,” Appl Compos Mater 21 March 2013

4. H.-S. Ahn J.-H. Kweon J.-H. Choi “Failure of Unidirectional-Woven Composite Laminated Pin-Loaded Joints,” Journal of Reinforced Plastics and Composites , 2005, no. 24:735

5. Three-Dimensional Stress Analyses in Composite Laminates with an Elastically Pinned Hole;Yang;Int J. Solids Struct.,2003

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. The failure stages of bolted double-lap metallic joints: experimental study;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2018-07-21

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