Author:
Guo Zhangxin,Han Xiaoping,Zhu Xiping
Publisher
Springer Science and Business Media LLC
Reference13 articles.
1. Ko, C.C., Lin, C.C.: Method for calculating the interlaminar stresses in symmetric laminates containing a circular hole. AIAA 30, 197–204 (1992)
2. Tolson, S., Zabaras, N.: Finite element analysis of progressive failure in laminated composite plates. Comput. Struct. 38, 361–367 (1991)
3. Zhen, Wu, Wanji, C.: Stress analysis of laminated composite plates with a circular hole according to a single-layer higher-order model. Compos. Struct. 90, 122–129 (2009)
4. Gliesche K, Feltin D.: Automated manufacture of textile reinforcements by tailored fiber placement. In: International symposium on composites manufacturing for aircraft structures, Flevoland pp 30–31. (2002)
5. Gliesche, K., Hubner, T., Orawetz, H.: Application of the tailored fiber placement process for a local reinforcement on an open-hole tensile plate from carbon/epoxy laminates. Compos. Sci. Technol. 63(1), 81–8 (2003)
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