Test on Composite Stiffened Panel with Different Stringer Cut-Outs under Uniaxial Tension

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Abstract:

This paper presents the tensile experiments of composite stiffened panel with three different stringer cut-out configurations. The strain distribution and delamination of the critical region near the stringer cut-out were studied. The influence from the different stringer cut-out configuration and geometric parameters on the strain distribution and delamination was evaluated via the comparison of experimental data, which can provide useful information to support further research and engineering applications.

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Periodical:

Advanced Materials Research (Volumes 718-720)

Pages:

1055-1059

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Online since:

July 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] Zhen Shen, Xiaojing Zhang. An introduction to design and verification for composite aircraft structures. Shanghai Jiao Tong University Press, Shanghai, (2011)

Google Scholar

[2] Christos Kassapoglou, Wanyi Yan. Design and analysis of composite structures with applications to aerospace structures. Shanghai Jiao Tong University Press, Shanghai, (2011)

Google Scholar

[3] Jinjuan Fan, Xiaoquan Cheng, Chunhu Tao. Failure analysis basics for polymer matrix composite components. National defense Industry Press, Beijing, (2011)

Google Scholar

[4] Beer F P et al. Mechanics of materials. McGraw – Hill Inc, New Yorks, (1992)

Google Scholar

[5] Mingjiu Xie. Joints for composite materials. Shanghai Jiao Tong University Press, Shanghai, (2011)

Google Scholar