J Shanghai Jiaotong Univ Sci

Journal of Shanghai Jiaotong University(Science) >

2021 , Vol. 26 >Issue 2: 218 - 230

DOI: https://doi.org/10.1007/s12204-021-2271-y

Energy Engineering, Mechanics & Materials

Experiment and Simulation of Impact Response of Woven CFRP Laminates with Different Stacking Angles

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  • (1. State Key Laboratory of Automotive Simulation and Control, Jilin University, Changchun 130022, China;
    2. CRRC Changchun Railway Vehicles Co., Ltd., Changchun 130062, China)

Online published: 2021-03-24

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Abstract

The effects of different laying angles on impact resistance and damage types of woven carbon fibrereinforced polymer (CFRP) laminates were studied. The drop hammer impact test and simulation analysis of woven CFRP laminates at four different velocities were carried out by means of the combination of experiment and explicit finite element analysis. The effect of impact velocity on damage pattern and fracture of woven CFRP laminates with eight layers and four laying angles (0°, 15°, 30°, and 45°) was studied by drop weight impact test, and the damage area of woven CFRP laminates with different laying angles was measured by ultrasonic nondestructive testing method. A user-defined material model was developed based on LS-DYNA to simulate the impact behavior of woven CFRP laminates. A finite element simulation model was established to effectively predict the complex damage evolution of woven CFRP laminates under low-speed impact loading. Its effectiveness was verified by impact response and damage crack pattern. The energy absorption and impact force of the laminated plate increase gradually from 0° to 45° in the laying angle of woven fabric. With the increase of laying angle from 0° to 45°, the length of fracture crack and the damage area increase. The developed model can accurately predict the impact properties of the composites.

Key words：  carbon fiber-reinforced polymer (CFRP); drop weight impact; damage propagation; stacking angle

Cite this article

ZHUANG Weimin (庄蔚敏), WANG Pengyue (王鹏跃), AO Wenhong (熬文宏), CHEN Gang (陈刚) . Experiment and Simulation of Impact Response of Woven CFRP Laminates with Different Stacking Angles[J]. Journal of Shanghai Jiaotong University(Science), 2021 , 26(2) : 218 -230 . DOI: 10.1007/s12204-021-2271-y

References

[1] ALAM P, MAMALIS D, ROBERT C, et al. The fatigue of carbon fibre reinforced plastics: A review [J].Composites Part B: Engineering, 2019, 166: 555-579.
[2] NAIK N K, BORADE S V, ARYA H, et al. Experimental studies on impact behaviour of woven fabric composites: Effect of impact parameters [J]. Journal of Reinforced Plastics and Composites, 2002, 21(15):1347-1362.
[3] ZHOU G. Damage mechanisms in composite laminates impacted by a flat-ended impactor [J]. Composites Science and Technology, 1995, 54(3): 267-273.
[4] KORICHO E G, KHOMENKO A, HAQ M, et al. Effect of hybrid (micro- and nano-) fillers on impact response of GFRP composite [J]. Composite Structures,2015, 134: 789-798.
[5] WALKER L, SOHN M S, HU X Z. Improving impact resistance of carbon-fibre composites through interlaminar reinforcement [J]. Composites Part A: Applied Science and Manufacturing, 2002, 33(6): 893-902.
[6] ATAS C, LIU D. Impact response of woven composites with small weaving angles [J]. International Journal of Impact Engineering, 2008, 35(2): 80-97.
[7] GRASSO M, XU Y, RAMJI A, et al. Low-velocity impact behaviour of woven laminate plates with fire retardant resin [J]. Composites Part B: Engineering,2019, 171(4): 1-8.
[8] CANTWELLWJ, MORTON J. Impact perforation of carbon fibre reinforced plastic [J]. Composites Science and Technology, 1990, 38(2): 119-141.
[9] L′OPEZ-PUENTE J, ZAERA R, NAVARRO C. Experimental and numerical analysis of normal and oblique ballistic impacts on thin carbon/epoxy woven laminates [J]. Composites Part A: Applied Science and Manufacturing, 2008, 39(2): 374-387.
[10] SARASINI F, TIRILL`O J, FERRANTE L, et al.Drop-weight impact behaviour of woven hybrid basaltcarbon/epoxy composites [J]. Composites Part B: Engineering,2014, 59: 204-220.
[11] DRANSFIELD K, BAILLIE C, MAI Y W. Improving the delamination resistance of CFRP by stitching: A review [J]. Composites Science and Technology, 1994,50(3): 305-317.
[12] ZHOU G, LLOYD J C, MCGUIRK J J. Experimental evaluation of geometric factors affecting damage mechanisms in carbon/epoxy plates [J]. Composites Part A:Applied Science and Manufacturing, 2001, 32(1): 71-84.
[13] SEVKAT E, LIAW B, DELALE F. Drop-weight impact response of hybrid composites impacted by impactor of various geometries [J]. Materials & Design,2013, 52: 67-77.
[14] SEVKAT E, LIAW B, DELALE F, et al.Drop-weight impact of plain-woven hybrid glassgraphite/toughened epoxy composites [J]. Composites Part A: Applied Science and Manufacturing, 2009,40(8): 1090-1110.
[15] HASHIN Z, ROTEM A. A fatigue failure criterion for fiber reinforced materials [J]. Journal of Composite Materials, 1973, 7(4): 448-464.
[16] HASHIN Z. Fatigue failure criteria for unidirectional fiber composites [J]. Journal of Applied Mechanics,1981, 48(4): 846-852.
[17] CHANG F K, CHANG K Y. Post-failure analysis of bolted composite joints in tension or shear-out mode failure [J]. Journal of Composite Materials, 1987,21(9): 809-833.
[18] PUCK A, SCH¨URMANN H. Failure analysis of FRP laminates by means of physically based phenomenological models [J]. Composites Science and Technology,1998, 58: 1045-1067.
[19] SIROMANI D, AWERBUCH J, TAN T M. Finite element modeling of the crushing behavior of thin-walled CFRP tubes under axial compression [J]. Composites Part B: Engineering, 2014, 64: 50-58.
[20] IANNUCCI L, ANKERSEN J. An energy based damage model for thin laminated composites [J]. Composites Science and Technology, 2006, 66(7/8): 934-951.
[21] IANNUCCI L, WILLOWSML. An energy based damage mechanics approach to modelling impact onto woven composite materials—Part I: Numerical models[J]. Composites Part A: Applied Science and Manufacturing,2006, 37(11): 2041-2056.
[22] IANNUCCI L. Progressive failure modelling of woven carbon composite under impact [J]. International Journal of Impact Engineering, 2006, 32(6): 1013-1043.
[23] FAGGIANI A, FALZON B G. Predicting low-velocity impact damage on a stiffened composite panel [J].Composites Part A: Applied Science and Manufacturing,2010, 41(6): 737-749.
[24] DONADON M V, IANNUCCI L, FALZON B G, et al.A progressive failure model for composite laminates subjected to low velocity impact damage [J]. Computers & Structures, 2008, 86(11/12): 1232-1252.
[25] XIAO X, BOTKIN M E, JOHNSON N L. Axial crush simulation of braided carbon tubes using MAT58 in LS-DYNA [J]. Thin-Walled Structures, 2009, 47(6/7):740-749.

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