Failure Analysis of Laminated Composite Plate Under Hygro-Thermo Mechanical Load and Optimisation

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Abstract

Failure analysis of laminated composite plates for different mechanical, thermo mechanical and hygro-thermo mechanical loads for different ply thicknesses, stacking sequences, fiber orientation angles and composite material systems is presented in the paper. A comparative study of different failure theories is also presented in the paper. The effect of fiber orientation angles on the first ply failure load is also studied. A hybrid composite laminate is developed based on the first ply failure load which minimizes weight and cost. The last ply failure load based on fully discounted method is calculated for different stacking sequences. An optimum composite material system and laminate layup is studied for a targeted strength ratio which minimizes weight.

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  • [1] Lee J.D. (1982): Three dimensional finite element analysis of damage accumulation in composite laminate. – Computers and Structures vol.15 No.3 pp.335-350.

  • [2] Reddy and Pandey (1987): A first ply failure analysis of composite laminate. – Computer and Structures vol.25 pp.371-393.

  • [3] Reddy and Pandey (1987): A post first ply failure analysis of composite laminate. – Proceedings of ASME 28th Structures Structural Dynamics and Materials Conference pp.788-797.

  • [4] Ochoa O.O. and Engblom J.J. (1987): Analysis of progressive failure in composites. – Composites Science and Technology vol.28 pp.87-102

  • [5] Reddy Y.S. and Reddy J.N. (1992): Linear and nonlinear failure analysis of composite laminates with transverse shear. – Composite Science and Technology vol.44 pp.227-255.

  • [6] Hwang W.C. and Sun C.T. (1989): Failure analysis of laminated composites by using iterative three-dimensional finite element method. – Computers and Structures vol.33 No.1 4 pp.1-47.

  • [7] Tan S.C. (1991): Progressive failure model for composite laminates containing opening. – Composite Materials vol.25 pp.556-577.

  • [8] Tan S.C. and Perez J. (1993): Progressive failure. of laminated composite with a hole under compressive loading. – J. Reinforced Plastics and Composites vol.12 pp.1043-1057.

  • [9] Tolsonand S. and Zasaras N. (1991): Finite element analysis of progressive failure in laminated composite plates. – Compurers and Structures vol.38 No.3 pp.361-376.

  • [10] Azizul Hakim Samsudin Ahmad KamilHussain and Jamaluddin Mahmud. (2015): Deformation and failure analysis of symmetric and antisymmetric graphite/epoxy laminate due to variations in fiber orientation. – ARPN Journal of Engineering and Applied Sciences vol.10 No.17.

  • [11] Jing-Fen Chen Evgeny V. Morozov and Krishnakumar Shankar (2014): Simulating progressive failure of composite laminates including in-ply and delamination damage effects. – Composites: Part A 61 pp.185–200.

  • [12] Jianyu Zhang DexuanQi Longwei Zhou Libin Zhao NingHua (2015): A progressive failure analysis model for composite structures in hygrothermal environments. – Composite Structures vol.133 pp.331–342.

  • [13] Taetragool U. Shah P.H. Halls V.A. Zheng J.Q. and Batra R.C. (2017): Stacking sequence optimization for maximizing the first failure initiation load followed by progressive failure analysis until the ultimate load. – Composite Structures vol.180 pp.1007–1021.

  • [14] Autar K. Kaw (2006): Mechanics of Composite Material. – CRC Press Taylor & Francis Group.

  • [15] Isaac M. and Daniel OriIshai (2013): Engineering Mechanics of Composite Materials. – Oxford University Press.

  • [16] Mustafa Akbulut and Fazil O. Sonmez (2011): Design optimization of laminated composites using a new variant of simulated annealing. – Computers and Structures vol.89 pp.1712–1724.

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