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Original Articles

A parametric study of stress concentration issues in unidirectional laminates

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Pages 1554-1569 | Received 09 Aug 2019, Accepted 30 Oct 2019, Published online: 13 Nov 2019

References

  • G. N. Savin. Stress Distribution around Holes. NASA Technical Translation, USA, 1970.
  • R. C. O. Góes, J. T. P. Castro, and M. A. Meggiolaro, “3D thickness effects around notch and crack tips,” Int. J. Fatigue, vol. 62, pp. 159–170, 2014. DOI: 10.1016/j.ijfatigue.2013.10.014.
  • S. G. Lekhniskii, Theory of Elasticity of an Anisotropic Body. Mir Publishers, Russia, 1981.
  • T. C. T. Ting, Anisotropic Elasticity: Theory and Applications. Oxford University Press, USA, 1996.
  • S. G. Lekhniskii, Anisotropic Plates. 3rd ed., Gordon and Breach Science Publishers, USA, 1987.
  • C. Hwu, Anisotropic Elastic Plates. Springer, USA, 2009.
  • S. C. Tan, “Laminated composites containing an elliptical opening. I. approximate stress analyses and fracture models,” J. Compos. Mater., vol. 21, no. 10, pp. 925–948, 1987. DOI: 10.1177/002199838702101004.
  • S. C. Tan, “Finite-width correction factors for anisotropic plate containing a central opening,” J. Compos. Mater., vol. 22, no. 11, pp. 1080–1097, 1988. DOI: 10.1177/002199838802201105.
  • M. O. Kaman, “Effect of fiber orientation on fracture toughness of laminated composite plates [0/θ]s,” Eng. Fract. Mech., vol. 78, no. 13, pp. 2521–2534, 2011. DOI: 10.1016/j.engfracmech.2011.06.005.
  • J. M. Whitney and R. J. Nuismer, “Stress fracture criteria for laminated composites containing stress concentration,” J. Compos. Mater., vol. 8, no. 3, pp. 253–265, 1974. DOI: 10.1177/002199837400800303.
  • M. Zappalorto and P. A. Carraro, “An engineering formula for the stress concentration factor of orthotropic composite plates,” Composite Part B, vol. 68, pp. 51–58, 2015. DOI: 10.1016/j.compositesb.2014.08.020.
  • R. D. B. Sevenois and S. Koussios, “Analytic methods for stress analysis of two-dimensional flat anisotropic plates with notches: an overview,” Appl. Mech. Rev., vol. 66, no. 6, pp. 060802, 2014. DOI: 10.1115/1.4027562.
  • E. V. Iarve, D. Mollenhauer, and R. Kim, “Theoretical and experimental investigation of stress redistribution in open hole composite laminates due to damage accumulation,” Composite Part A, vol. 36, no. 2, pp. 163–171, 2005. DOI: 10.1016/j.compositesa.2004.06.011.
  • D. Mollenhauer, E. V. Iarve, R. Kim, and B. Langley, “Examination of ply cracking in composite laminates with open holes: A moiré interferometric and numerical study,” Composite Part A, vol. 37, no. 2, pp. 282–294, 2006. DOI: 10.1016/j.compositesa.2005.06.004.
  • R. M. O’Higgins, M. A. McCarthy, and C. T. McCarthy, “Comparison of open hole tension characteristics of high strength glass and carbon fibre-reinforced composite,” Compos. Sci. Technol., vol. 68, pp. 2770–2778, 2008. DOI: 10.1016/j.compscitech.2008.06.003.
  • J. Lee and C. Soutis, “Measuring the notched compressive strength of composite laminates: Specimen size effects,” Compos. Sci. Technol., vol. 68, no. 12, pp. 2359–2366, 2008. DOI: 10.1016/j.compscitech.2007.09.003.
  • J. Cugnoni et al., “Towards aerospace grade thin-ply composites: Effect of ply thickness, fibre, matrix and interlayer toughening on strength and damage tolerance,” Compos. Sci. Technol., vol. 168, pp. 467–477, 2018. DOI: 10.1016/j.compscitech.2018.08.037.
  • C. Furtado, A. Arteiro, G. Catalanotti, J. Xavier, and P. P. Camanho, “Selective ply-level hybridisation for improved notched response of composite laminates,” Compos. Struct., vol. 145, pp. 1–14, 2016. DOI: 10.1016/j.compstruct.2016.02.050.
  • S. Zhou, J. Zhang, Y. Sun, and K. Tian, “Experimental and numerical investigation of open hole carbon fiber composite laminates under compression with three different stacking sequences,” J. Mater. Res. Technol., vol. 8, no. 3, pp. 2957–2968, 2019. DOI: 10.1016/j.jmrt.2019.05.003.
  • M. Kawai, K. Watanabe, H. Hoshi, E. Hara, and Y. Iwahori, “Effect of specimen size on longitudinal strength of unidirectional carbon/epoxy composite laminates (part 2, splitting strength),” Adv. Compos. Mater., vol. 28, no. Suppl 2, pp. 73–100, 2019. DOI: 10.1080/09243046.2018.1458270.
  • S. W. Tsai and J. D. D. Melo, “An invariant-based theory of composites,” Compos. Sci. Technol., vol. 100, pp. 237–243, 2014. DOI: 10.1016/j.compscitech.2014.06.017.
  • Y. Huang et al., “Effects of an Open Hole on the Biaxial Strengths of Composite Laminates,” J. Compos. Mater., vol. 44, pp. 2429–2445, 2010.
  • U. Kureemun, M. Ridha, and T. E. Tay, “Biaxial tensile-compressive loading of unnotched and open-hole carbon epoxy crossply laminates,” J. Compos. Mater., vol. 49, no. 23, pp. 2817–2837, 2015. DOI: 10.1177/0021998314555043.
  • P. D. Shah, J. D. D. Melo, C. A. Cimini, Jr, and M. Ridha, “Evaluation of notched strength of composite laminates for structural design,” J. Compos. Mater., vol. 44, no. 20, pp. 2381–2392, 2010. DOI: 10.1177/0021998310372713.
  • J. L. Y. Tan, V. S. Deshpande, and N. A. Fleck, “Prediction of failure in notched carbon-fibre-reinforced polymer laminates under multi-axial loading,” Phil. Trans. R. Soc. A., vol. 374, no. 2071, pp. 20150273, 2016. DOI: 10.1098/rsta.2015.0273.
  • B. Y. Chen, T. E. Tay, P. M. Baiz, and S. T. Pinho, “Numerical analysis of size effects on open-hole tensile composite laminates,” Composite Part A, vol. 47, pp. 52–62, 2013. DOI: 10.1016/j.compositesa.2012.12.001.
  • Z. C. Su, T. E. Tay, M. Ridha, and B. Y. Chen, “Progressive damage modeling of open-hole composite laminates under compression,” Compos. Struct., vol. 122, pp. 507–517, 2015. DOI: 10.1016/j.compstruct.2014.12.022.
  • G. Sadeghi, H. Hosseini-Toudeshky, and B. Mohammadi, “An investigation of matrix cracking damage evolution in composite laminates – Development of an advanced numerical tool,” Compos. Struct., vol. 108, pp. 937–950, 2014. DOI: 10.1016/j.compstruct.2013.10.007.
  • M. M. Moure et al., “Damage evolution in open-hole laminated composite plates subjected to in-plane loads,” Compos. Struct., vol. 133, pp. 1048–1057, 2015. DOI: 10.1016/j.compstruct.2015.08.045.
  • A. P. K. Joseph, P. Davidson, and A. M. Waas, “Open hole and filled hole progressive damage and failure analysis of composite laminates with a countersunk hole,” Compos. Struct., vol. 203, pp. 523–538, 2018. DOI: 10.1016/j.compstruct.2018.06.120.
  • A. Farrokhabadi and R. Babaei, “Development of an integrated micro macro model for anticipating matrix cracking evolution and fiber breakage in the laminated composite containing an open hole,” Eng. Fract. Mech., vol. 211, pp. 161–179, 2019. DOI: 10.1016/j.engfracmech.2019.02.004.
  • L. L. Vignoli, M. A. Savi, P. M. C. L. Pacheco, and A. L. Kalamkarov, “Comparative analysis of micromechanical models for the elastic composite laminae,” Composites Part B, vol. 174, pp. 106961, 2019. DOI: 10.1016/j.compositesb.2019.106961.
  • C. Furtado, A. Arteiro, M. A. Bessa, B. L. Wardle, and P. P. Camanho, “Prediction of size effects in open-hole laminates using only the Young’s modulus, the strength, and the R-curve of the 0 ply,” Composites: Part A, vol. 101, pp. 306–317, 2017. DOI: 10.1016/j.compositesa.2017.04.014.
  • L. L. Vignoli and M. A. Savi, “Multiscale failure analysis of cylindrical composite pressure vessel: A parametric study,” Latin Am. J. Solids Struct., vol. 15, no. 11, pp. e63, 2018. DOI: 10.1590/1679-78254323.
  • I. V. Andrianov, J. Awrejcewicz, and V. V. Danishevs’kyy, Asymptotical Mechanics of Composites - Modelling Composites Without FEM. Springer, 2018.
  • M. Zappalorto and P. A. Carraro, “Stress distributions for blunt cracks and radiused slits in anisotropic plates under in-plane loadings,” Int. J. Solids Struct., vol. 56-57, pp. 136–141, 2015. DOI: 10.1016/j.ijsolstr.2014.11.024.
  • M. Zappalorto, “On the stress state in rectilinear anisotropic thick plates with blunt cracks,” Fatigue Fract. Eng. Mater. Struct., vol. 40, pp. 103–119, 2017. DOI: 10.1111/ffe.12479.
  • N. Bonora, M. Costanzi, and M. Marchetti, “On closed form solution for the elastic stress field around holes in orthotropic composite plates under in-plane stress conditions,” Compos. Struct., vol. 25, no. 1–4, pp. 139–156, 1993. DOI: 10.1016/0263-8223(93)90160-R.
  • N. Bonora, M. Costanzi, and M. Marchetti, “A computational procedure to calculate stress-strain field around simple shape holes in composite laminates,” Compos. Struct., vol. 53, no. 5, pp. 1167–1179, 1994. DOI: 10.1016/0045-7949(94)90164-3.
  • A. L. Kalamkarov and A. Georgiades, “Modeling of smart composites on account of actuation, thermal conductivity and hygroscopic absorption,” Composites Part B, vol. 33, no. 2, pp. 141–152, 2002. DOI: 10.1016/S1359-8368(01)00062-2.
  • A. Puck and H. Schürmann, “Failure analysis of FRP laminates by means of physically based phenomenological models,” Compos. Sci. Technol., vol. 58, no. 7, pp. 1045–1067, 1998. DOI: 10.1016/S0266-3538(96)00140-6.
  • P. D. Soden, A. S. Kaddour, and M. J. Hinton, “Recommendations for designers and researchers resulting from the world-wide failure exercise,” Compos. Sci. Technol., vol. 64, no. 3–4, pp. 589–604, 2004. DOI: 10.1016/S0266-3538(03)00228-8.
  • A. S. Kaddour and M. J. Hinton, “Maturity of 3D failure criteria for fibre reinforced composites: Comparison between theories and experiments: Part B of WWFE-II,” J. Compos. Mater., vol. 47, no. 6-7, pp. 925–966, 2013. DOI: 10.1177/0021998313478710.
  • I. S. Sokolnikoff, Mathematical Theory of Elasticity. 2nd ed., McGraw-Hill Book Company, USA, 1956.
  • D. M. Barnett and J. Lothe, “Synthesis of the sextic and the integral formalism for dislocation, green’s function and surface waves in anisotropic elastic solids,” Phys. Norv., vol. 7, pp. 13–19, 1973.
  • R. G. Cuntze and A. Freund, “The predictive capability of failure mode concept-based strength criteria for multidirectional laminates,” Compos. Sci. Technol., vol. 64, no. 3–4, pp. 343–377, 2004. DOI: 10.1016/S0266-3538(03)00218-5.
  • H. M. Deuschle and A. Puck, “Application of the Puck failure theory for fibre-reinforced composites under three-dimensional stress: Comparison with experimental results,” J. Compos. Mater., vol. 47, no. 6-7, pp. 827–846, 2013. DOI: 10.1177/0021998312462158.
  • VDI Guideline. 2014 Part 3: Development of Fibre-Reinforced-Plastics Components, Analysis, Issue German/English. Berlin: Beuth-Verlag, 2006.
  • M. Knops, Analysis of Failure in Fiber Polymer Laminates - The Theory of Alfred Puck. Springer, Germany, 2008.
  • A. S. Kaddour and M. J. Hinton, “Input data for test cases used in benchmarking triaxial failure theories of composites,” J. Compos. Mater., vol. 46, no. 19–20, pp. 2295–2312, 2012. DOI: 10.1177/0021998312449886.
  • C. S. Lee, J. H. Kim, S. K. Kim, D. M. Ryu, and J. M. Lee, “Initial and progressive failure analyses for composite laminates using Puck failure criterion and damage-coupled finite element method,” Compos. Struct., vol. 121, pp. 406–419, 2015. DOI: 10.1016/j.compstruct.2014.11.011.
  • H. Junshan et al., “Stress analysis and damage evolution in individual plies of notched composite laminates subjected to in-plane loads,” Chin. J. Aeronaut., vol. 30, pp. 447–460, 2017. DOI: 10.1016/j.cja.2016.10.022.
  • P. P. Camanho and F. L. Matthews, “A progressive damage model for mechanically fastened joints in composite laminates,” J. Compos. Mater., vol. 33, no. 24, pp. 2248–2280, 1999. DOI: 10.1177/002199839903302402.
  • M. V. Angelo, M. L. Ribeiro, and V. Tita, “A computational framework for predicting onset and crack propagation in composite structures via eXtended Finite Element Method (XFEM),” Latin Am. J. Solids Struct., vol. 15, no. 11, e70, pp. 1–14, 2018. DOI: 10.1590/1679-78254301.

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