Abstract
The elasto-plastic postbuckling of fiber metal laminated beams with delamination and the energy release rate along the delamination front are discussed in this paper. Considering geometrical nonlinearity, thermal environment and geometrical initial imperfection, the incremental nonlinear equilibrium equations of delaminated fiber metal laminated beams are established, which are solved using the differential quadrature method and iterative method. Based on these, according to the J-integral theory, the elasto-plastic energy release rate is studied. The effects of some important parameters on the elasto-plastic postbuckling behavior and energy release rate of the aramid reinforced aluminum laminated beams are discussed in details.
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Tamer Sinmazcelik and Egemen Avcu, A review: Fibre metal laminates, background, bonding types and applied test methods. Materials and Design, 2011, 32: 3671–3685.
Schut, J.E. and Alderliesten, R.C., Delamination Growth Rate at Low and Elevated Temperatures in Glare. 25th international congress of the aeronautical sciences, 2006: 3–8.
Remmers, J.J.C. and de Borst, R., Delamination buckling of fibre-metal laminates. Composites Science and Technology, 2001, 61: 2207–2213.
Khan, S.U., Alderliesten, R.C. and Benedictus, R., Delamination growth in fibre metal laminates under variable amplitude loading. Composites Science and Technology, 2009, 69(15–16): 2604–2615.
Khan, S.U., Alderliesten, R.C., Rans, C.D. and Benedictus, R., Application of a modified wheeler model to predict fatigue crack growth in fibre metal laminates under variable amplitude loading. Engineering Fracture Mechanics, 2010, 77(9): 1400–1416.
Khan, S.U., Alderliesten, R.C. and Benedictus, R., Delamination in fiber metal laminates (GLARE) during fatigue crack growth under variable amplitude loading. International Journal of Fatigue, 2011, 33(9): 1292–1303.
de Vries, T.J., Vlot, A. and Hashagen, F., Delamination behavior of spliced fiber metal laminates. Part 1. Experimental results. Composite Structures, 1999, 46: 131–145.
Hashagen, F., Vlot, A. and de Vries, T.J., Delamination behavior of spliced fiber metal laminates. Part 2. Numerical investigation. Composite Structures, 1999, 46: 147–162.
Chen, J.L. and Sun, C.T., Modeling of orthotropic elastic-plastic properties of ARALL laminates. Composites Science and Technology, 1989, 36: 321–337.
Esfandiar, H., Analysis of elastic-plastic behavior of fiber metal laminates subjected to in-plane tensile loading, International Journal of Advanced Design and Manufacturing Technology, 2011, 5: 61–69.
Aboudi, J. and Paley, M., Plastic buckling of ARALL plates. Composite Structures, 1992, 22: 217–221.
Vo, T.P., Guan, Z.W. Cantwell, W.J. and Schleyer, G.K., Low-impulse blast behaviour of fibre-metal laminates. Composite Structures, 2012, 94: 954–965.
Kenaga, D., Doyle, J.F. and Sun, C.T., The characterization of boron/aluminum composite in the nonlinear range as an orthotropic elastic-plastic material. Journal of Composite Materials, 1987, 21: 516–531.
Fu, Y.M. and Tian, Y.P., The elasto-plastic damage constitutive relations of orthotropic materials. Chinese Journal of Theoretical and Applied Mechanics, 2009, 41: 67–75.
Rice, J.R., A path independent integral and the approximate analysis of concentration by notches and cracks. Journal of Applied Mechanics, 1968, 35: 397–386.
Bert, C.W. and Malik, M., Differential quadrature method in computational mechanics: a review. Applied Mechanics Review. 1996, 49: 1–28.
Simitses, G.J., Sallam, S. and Yin, W.L., Effect of delamination of axially loaded homogeneous laminated plates. AIAA Journal, 1985, 23: 1437–1444.
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Project supported by the National Natural Science Foundation of China (No. 11272117).
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Fu, Y., Chen, Y. & Shao, X. Analysis of Elasto-Plastic Postbuckling and Energy Release Rate for Delaminated Fiber Metal Laminated Beams in Thermal Environment. Acta Mech. Solida Sin. 28, 693–705 (2015). https://doi.org/10.1016/S0894-9166(16)30010-6
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DOI: https://doi.org/10.1016/S0894-9166(16)30010-6