Dynamic Impact Analysis for Ex Situ Toughened Composite Laminates

Li Peng Liu; Xue Feng An; Ming Zhang; Xiao Su Yi

doi:10.4028/www.scientific.net/AMM.152-154.579

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 152-154Dynamic Impact Analysis for Ex Situ Toughened...

Dynamic Impact Analysis for Ex Situ Toughened Composite Laminates

Abstract:

Dynamic impact loading/energy-absorbed response curves of controlled T800/5228A laminates and corresponding “Ex-situ” toughened T800/5228E laminates were contrastively studied. It was concluded that both Hertzian failure loading and the maximum loading were improved by interlaminar toughening, based on the enhancement of Mode II crack strength. T800/5228E laminates presented less damage area than T800/5228A laminates under equivalent impact energy, but consumed more total energy, and further study show that serious external damage on the surface of T800/5228E lamiantes may be responsible for the more impacted energy consumed .

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Periodical:

Applied Mechanics and Materials (Volumes 152-154)

Pages:

579-584

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.152-154.579

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Online since:

January 2012

Authors:

Li Peng Liu, Xue Feng An, Ming Zhang, Xiao Su Yi

Keywords:

Dynamic Impact Response Curves, Ex Situ Toughening, Hertzian Failure, Maximum Response Loading, Mode II Crack Strength

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References

[1] Qunfeng Cheng, Zhengping Fang, Yahong Xu and Xiaosu Yi. Improvement of the Impact Damage Resisitance of BMI/Graphite Laminates by the Ex-Situ Method[J]. High. Performance Polymers, Vol 18, no. 6, P907-917, (2006).

DOI: 10.1177/0954008306068296

Google Scholar

[2] Dong Hwee Kim, Jisu Choi, Young Taik Hong, Sung Chul Kim, Phase separation and morphology control of polymer blend membranes of sulfonated and nonsulfonated polysulfones for direct methanol fuel cell application. [J]. Journal of Membrane Science 299 (2007).

DOI: 10.1016/j.memsci.2007.04.014

Google Scholar

[3] Qunfeng Cheng, Zhengping Fang, Xiao-Su Yi, Xuefeng An, Bangming Tang, Yahong Xu. Ex-situ, Concept for Toughening the RTMable BMIMatrix Composites, Part I: Improving the InterlaminarFracture Tougheness[J]. Journal of Applied Polymer Science, Vol. 109, 1625–1634 (2008).

DOI: 10.1002/app.27868

Google Scholar

[4] Lipeng LIU, Xuefeng AN, Ming Zhang, Xiaosu Yi. Improving Compression after Impact of T800H/5228A Composite Laminates through Interlaminate Toughening[J]. Advanced materials research. Accepted.

DOI: 10.4028/www.scientific.net/amm.182-183.41

Google Scholar

[5] Tien-Wei Shyr, Yu-Hao Pan. Impact resistance and damage characteristics of composite laminates[J]. Composite Structures 62 (2003) 193~203.

DOI: 10.1016/s0263-8223(03)00114-4

Google Scholar

[6] Sandrine Petit, Christophe Bouvet, Alain Bergerot, Jean-Jacques Barrau. Impact and compression after impact experimental study of a composite laminate with a cork thermal shield. Composites Science and Technology 67 (2007) 3286–3299.

DOI: 10.1016/j.compscitech.2007.03.032

Google Scholar

[7] S. A. Hitchen, R. M. J. Kemp. The effect of stacking sequence on impact damage in a carbon fibre/epoxy composite[J]. Composites 26 (1995) 207~214.

DOI: 10.1016/0010-4361(95)91384-h

Google Scholar

[8] G. Caprino, V. Lopresto, C. Scarponi, G. Briotti. Influence of material thickness on the response of carbon fabric/epoxy panels to low velocity impact[J]. Composites Science and Technology 59 (1999) 2279-2286.

DOI: 10.1016/s0266-3538(99)00079-2

Google Scholar

[9] Standard test method for measuring the damage resistance of a fibrereinforced polymer matrix composite to a drop-weight impact event, Tech. rep. West Conshohocken (PA, USA): American Society for Testing andMaterials (ASTM), ASTM D 7136/D 7136M-05, (2005).

DOI: 10.1520/d7136_d7136m-12

Google Scholar

[10] HB 7403-96 (Standard of Chinese Aviation). Testing Method for Mode II Interlaminar Fracture Tougheness of Carbon Fiber Reinforced Plastics; 1996 (in Chinese).

Google Scholar

[11] Schoeppner GA, Abrate S. Delamination threshold loading for low velocity impact on composite laminates. Composites: part A 2000; 31: 903-15.

DOI: 10.1016/s1359-835x(00)00061-0

Google Scholar

[12] Giovanni Belingardi, Roberto Vadori. Low velocity impact tests of laminate glass-fiber-epoxy matrix composite material plates[J]. International Journal of Impact Engineering 27 (2002) 213-29.

DOI: 10.1016/s0734-743x(01)00040-9

Google Scholar

[13] CHENG Xiao-quan. Degree Thesis of Beijing Univ. of Aero. and Astro in chinese, (1998).

Google Scholar

[14] Lipeng LIU, Xuefeng AN, Ming Zhang, Xiaosu Yi Improving Compression after Impact of T800H/5228A Composite Laminates through Interlaminate Toughening[J]. Advanced material research, accepted.

DOI: 10.4028/www.scientific.net/amm.182-183.41

Google Scholar