Finite Element Analysis of Woven Fabric Laminates Structural Strength

Gang Tong; Tong Fei Liu

doi:10.4028/www.scientific.net/AMR.785-786.199

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 785-786Finite Element Analysis of Woven Fabric Laminates...

Finite Element Analysis of Woven Fabric Laminates Structural Strength

Abstract:

The characteristics of the woven fabric laminates structure is described. The steps and method of building the woven fabric laminates structure finite element model in MSC Patran is provided. The accuracy of this method is verified by a group of finite element calculation and experimental data.

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Periodical:

Advanced Materials Research (Volumes 785-786)

Pages:

199-203

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.785-786.199

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Cite this paper

Online since:

September 2013

Authors:

Gang Tong, Tong Fei Liu

Keywords:

Carbon Fiber Cloth, Composite Material, Finite Element, Laminated Structure, MSC Nastran, MSC Patran

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References

[1] GuanlinShen, GengkaiHu. Mechanics of composite materials [M]. Beijing: Tsinghua University press, (2006).

Google Scholar

[2] GuoqingLiu. Finite element model updating technique of composite structures [D]. Shanghai: Shanghai Jiao Tong University, 2011: 1-3.

Google Scholar

[3] ZhufengYue, FushengWang, PeiyanWang etc. Aircraft composite structure analysis and optimization design [M]. Beijing: Science Press, (2011).

Google Scholar

[4] KaiLong, ChangzhiJia, BaofengLi etc. Patran2010 and Nastran2010 finite element analysis from entry to the master [M]. 2 edition. Beijing: Mechanical Industry Press, (2011).

Google Scholar

[5] China Institute of Aeronautics. Composite decoupling unit design handbook [M]. Beijing: Aviation Industry Press,. 2011: 75.

Google Scholar

[6] Michael C.Y. Niu. The utility aircraft structure stress analysis and the size design of [M]. ZhenyuFeng, XiaoquanCheng, JikuiZhang, trans. Beijing: Aviation Industry Press, (2008).

Google Scholar

[7] Michael C.Y. Niu. Practical aircraft structural engineering design of [M]. XiaoquanCheng, trans. Beijing: Aviation Industry Press, (2008).

Google Scholar

[8] JianhuaFan, QingxiongYang. The elastic modulus of the composite random calculation model [J]. Journal of composite materials. 1998, 15 (4): 134-138.

Google Scholar

[9] LijuanXia, XiandingJin, XiangbaoWang. Calculation of the equivalent of honeycomb sandwich plates for satellite structure[J]. Journal of Shanghai Jiao Tong University. 2003, 37 (7): 999-1001.

Google Scholar

[10] LiushengHuang. Composite sandwich plate hull structure strength analysis on the methods of [D]. Harbin: Harbin Engineering University, 2009: 17-24.

Google Scholar