Analysis of Nonlinear Shear Deformations in CFRP and GFRP Textile Laminates

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Carbon fibre-reinforced polymer (CFRP) and glass fibre-reinforced polymer (GFRP) woven composites are widely used in aerospace, automotive and construction components and structures thanks to their lower production costs, higher delamination and impact strengths. They can also be used in various products in sports industry. These products are exposed to different in-service conditions such as large tensile and bending deformations. Composite materials, especially ±45° symmetric laminates subjected to tensile loads, exhibit significant material as well as geometric non-linearity before damage initiation, particularly with respect to shear deformations. Such a nonlinear response needs adequate means of analysis and investigation, the major tools being experimental tests and numerical simulations. This research deals with modelling the nonlinear deformation behaviour of CFRP and GFRP woven laminates subjected to in-plane tensile loads. The mechanical behaviour of woven laminates is modelled using nonlinear elasto-plastic as well as material models for fabrics in commercial finite-element code Abaqus. A series of tensile tests is carried out to obtain an in-plane full-field strain response of [+45/-45]2s CFRP and GFRP laminates using digital image correlation technique according to ASTM D3518/D3518M-94. The obtained results of simulations are in good agreement with experimental data.

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363-368

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August 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] C. Hochard, J. Payan, C. Bordreuil, International Journal of Fatigue, 28 (2006) 1270-1276.

Google Scholar

[2] G. Ernst, M. Vogler, C. Hühne, R. Rolfes, Composites Science and Technology, 70 (2010) 61-72.

DOI: 10.1016/j.compscitech.2009.09.006

Google Scholar

[3] G. Odegard, K. Searles, M. Kumosa, Composites Science and Technology, 61 (2001) 2501-2510.

Google Scholar

[4] S. Ogihara, K.L. Reifsnider, Applied Composite Materials, 9 (2002) 249-263.

Google Scholar

[5] A. Tabiei, I. Ivanov, International Journal of Non-Linear Mechanics, 39 (2004) 175-188.

Google Scholar

[6] C. Hochard, S. Miot, N. Lahellec, F. Mazerolle, M. Herman, J.P. Charles, Composites Part A, 40 (2009) 1017-1023.

DOI: 10.1016/j.compositesa.2008.02.018

Google Scholar

[7] D.R. Hufner, M.L. Accorsi, Composite Structures, 89 (2009) 177-185.

Google Scholar

[8] L. Xing, K.L. Reifsnider, X. Huang, Composites Science and Technology, 69 (2009) 780-784.

Google Scholar

[9] C.T. Sun, J. Tao, Composites Science and technology, 58 (1998) 1125-1136.

Google Scholar

[10] ASTM D3518/D3518M-94: Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45° Laminate (2007).

DOI: 10.1520/d3518_d3518m-94e01

Google Scholar

[11] M.A. Sutton, W.J. Wolters, W.H. Peters, W.F. Ranson, S.R. McNeill, Image and Vision Computing, 1 (1983) 133-139.

DOI: 10.1016/0262-8856(83)90064-1

Google Scholar

[12] T.C. Chu, W.F. Ranson, M.A. Sutton, Experimental Mechanics, 25 (1985) 232-244.

Google Scholar

[13] D. Ivanov, S. Ivanov, S. Lomov, I. Verpoest, Optics and Lasers in Engineering, 47 (2009) 360-370.

DOI: 10.1016/j.optlaseng.2008.05.013

Google Scholar

[14] S.V. Lomov, D.S. Ivanov, I. Verpoest, M. Zako, T. Kurashiki, H. Nakai, J. Molimard, A. Vautrin, Composites Part A, 39 (2008) 1218-1231.

DOI: 10.1016/j.compositesa.2007.09.011

Google Scholar

[15] F.P. Van Der Meer, L.J. Sluys, Journal of Composite Materials, 43 (2009) 2131.

Google Scholar

[16] Hibbit, Karlsson, Sorensen, in, ABAQUS User's Manual, Version 6. 10, Michigan, USA, (2010).

Google Scholar