Ply Thickness’ Effect on Composite Laminate under Low-Velocity Impact

Xiang Cheng Luo; Tao Zhang; Qing Shan Wang

doi:10.4028/www.scientific.net/AMR.989-994.74

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 989-994Ply Thickness’ Effect on Composite Laminate under...

Ply Thickness’ Effect on Composite Laminate under Low-Velocity Impact

Abstract:

Based on the two-dimensional Hashin failure criteria and the introduction of material degradation damage factor, low-speed impact model of composite laminated plate was established by ABAQUS with fiber and matrix’s failure modes being taken into consideration. The mode is verified by referring to Karakuzu test. Next, it analyzes single ply thickness’ effect on laminated plate’s response and damaged under low-velocity impact. The result shows that with the thickness increasing, impact contact time and laminated plate impact point’s deflection displacement reduce, while the impact force and volatile shocks are more obvious.

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Periodical:

Advanced Materials Research (Volumes 989-994)

Pages:

74-78

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.989-994.74

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Cite this paper

Online since:

July 2014

Authors:

Xiang Cheng Luo*, Tao Zhang, Qing Shan Wang

Keywords:

Dynamic Response, Laminate, Low Velocity Impact (LVI), Ply Thickness

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* - Corresponding Author

References

[1] De Moura M, Marques A T. Prediction of low velocity impact damage in carbon–epoxy laminates[J]. Composites Part A: Applied Science and Manufacturing, 2002, 33(3): 361-368.

DOI: 10.1016/s1359-835x(01)00119-1

Google Scholar

[2] Choi H Y, Wu H Y T, Chang F K. A new approach toward understanding damage mechanisms and mechanics of laminated composites due to low-velocity impact: Part II—analysis[J]. Journal of Composite Materials, 1991, 25(8): 1012-1038.

DOI: 10.1177/002199839102500804

Google Scholar

[3] Shi Y, Swait T, Soutis C. Modelling damage evolution in composite laminates subjected to low velocity impact[J]. Composite Structures, 2012, 94(9): 2902-2913.

DOI: 10.1016/j.compstruct.2012.03.039

Google Scholar

[4] Yongdong Wu, Weifang Zhong, Qing Zhu. Research on the low velocity impact response of SMA hybrid composite plate[J]. Journal of vibration and shock, 2004, 23(1): 70-73.

Google Scholar

[5] Fuoss E, Straznicky P V, Poon C. Effects of stacking sequence on the impact resistance in composite laminates—Part 1: parametric study[J]. Composite Structures, 1998, 41(1): 67-77.

DOI: 10.1016/s0263-8223(98)00036-1

Google Scholar

[6] Karakuzu R, Erbil E, Aktas M. Impact characterization of glass/epoxy composite plates: an experimental and numerical study[J]. Composites Part B: Engineering, 2010, 41(5): 388-395.

DOI: 10.1016/j.compositesb.2010.02.003

Google Scholar

[7] ABAQUS 6. 10-1 Documentation. Abaqus analysis user's manual; 2010. p. (21. 3. 1-1) –(21. 3. 2-4).

Google Scholar