Structural Engineering and Mechanics

  • 제63권5호
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  • Pages.597-605
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  • 2017
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  • 1225-4568(pISSN)
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  • 1598-6217(eISSN)
테크노프레스 (Techno-Press)
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DOI QR코드

DOI QR Code

Delamination of a composite laminated under monotonic loading

  • Achache, Habib (Department of Materials Engineering, University Dr Yahia Fares of Medea) ;
  • Benzerdjeb, Abdelouahab (Department of Mechanical Engineering University of Science and Technology Oran Mohammed Boudiaf (USTO)) ;
  • Mehidi, Abdelkader (Laboratory of Mechanical and Physical of Materials (LMPM), University Djillali Liabes of Sidi Bel Abbes) ;
  • Boutabout, Benali (Laboratory of Mechanical and Physical of Materials (LMPM), University Djillali Liabes of Sidi Bel Abbes) ;
  • Ouinas, Djamel (Laboratory of Numerical and Experimental Modeling of Mechanical Phenomena, University of Mostaganem)
  • 투고 : 2016.12.12
  • 심사 : 2017.05.05
  • 발행 : 2017.09.10
⟨ 이전 논문 다음 논문 ⟩

초록

Our work aims to analyze using the finite element method the evolution of the stress intensity factor (SIF) parameter K of three laminated folded plates stacks [$+{\alpha}$, $-{\alpha}$], made of the same epoxy matrix and different reinforcement fibers (boron, graphite and glass). Our results show that the angle of orientation of the boron/epoxy composite has no great influence on the variation of the parameter KI. Compared to composite graphite/epoxy and glass/epoxy, the laminated composite boron/epoxy reduces more the SIF KI in the middle of the plate for angles $0^{\circ}{\leq}{\alpha}{\leq}30^{\circ}$.

키워드

참고문헌

  1. Anderson, T.L. (2005), Fracture Mechanics-Fundamentals and Applications, 3rd Edition, CRC Press.
  2. Haneef, M., Sa, R. and Ali, M.M. (2011), "Studies on delaminating effects on stress development in composite structures", Proceedings of the World Congress on Engineering Vol. III WCE, July, London, U.K.
  3. Jayatilake, I.N., Karunasena, W. and Lokuge, W. (2016), "Finite element based dynamic analysis of multilayer fibre composite sandwich plates with interlayer delaminations. Indunil", Adv. Aircraft Spacecraft Sci., 3(1), 15-28. https://doi.org/10.12989/aas.2016.3.1.015
  4. Kutlu, Z. and Chang, F.K. (1992), "Modeling compression failure of laminated composites containing multiple through-the-width delaminations", J. Compos. Mater., 26(3), 350e86. https://doi.org/10.1177/002199839202600303
  5. Li, D.H., Liu, Y. and Zhang, X. (2015), "An extended Layerwise method for composite laminated beams with multiple delaminations and matrix cracks", Int. J. Numer. Meth. Eng., 101, 407e34. https://doi.org/10.1002/nme.4803
  6. Liu, L., Zhang, J., Wang, H. and Guan, Z. (2015), "Mechanical behavior of the composite curved laminates in practical applications". Steel Compos. Struct., 19(5), 1095-1113. https://doi.org/10.12989/scs.2015.19.5.1095
  7. Liu, Y. and Shu, D.W. (2015), "Effects of edge crack on the vibration characteristics of delaminated beams", Struct. Eng. Mech., 53(4), 767-780. https://doi.org/10.12989/sem.2015.53.4.767
  8. Maimi, P., Camanho, P.P., Mayugo, J.A. and Turon, A. (2011), "Matrix cracking and delamination in laminated composites", Part I: Ply constitutive law, first ply failure and onset of delamination", Mech. Mater., 43, 169-185. https://doi.org/10.1016/j.mechmat.2010.12.003
  9. Product Dassault Systemes Simulia Corp (2012), ABAQUS Standard Version 6.12, Providence, RI, USA.
  10. Rooke, D.P. and Cartwright, D.J. (1976), "Compendium of stress intensity factors", HMSO Ministry of Defence, Procurement Executive.
  11. Seo, D.C. and Lee, J.J. (2002), "Fatigue crack growth behavior of cracked aluminum platerepaired with composite patch", Compos. Struct., 57, 323-330. https://doi.org/10.1016/S0263-8223(02)00095-8
  12. Short, G.J., Guild, F.J. and Pavier, M.J. (2001), "The effect of delamination geometry on the compressive failure of composite laminates", Compos. Sci. Technol., 61, 2075e86. https://doi.org/10.1016/S0266-3538(01)00134-8
  13. Suemasu, H., Sasaki, W., Ishikawa, T. and Aoki, Y. (2008), "A numerical study on compressive behavior of composite plates with multiple circular delaminations considering delamination propagation", Compos. Sci. Technol., 68, 2562-2567. https://doi.org/10.1016/j.compscitech.2008.05.014
  14. Tada, H., Paris, P. and Irwin, G. (2000), The Stress Analysis of Cracks Handbook, 3rd Edition, ASME Press.
  15. Todo, M. and Jar, P.Y. (1998), "Study of mode-I interlaminar crack growth in DCB specimens of fibre-reinforced composites", Compos. Sci. Technol., 58, 105-118. https://doi.org/10.1016/S0266-3538(97)00102-4
  16. Wang, X.W., Lezica, I.P., Harris, J.M., Guild, F.J. and Pavier, M.J. (2005), "Compressive failure of composite laminates containing multiple delaminations", Compos. Sci. Technol., 65, 191e200. https://doi.org/10.1016/j.compscitech.2004.06.010
  17. Zhao, L., Gong, Y., Zhang, J., Chen, Y. and Fei, B. (2014), "Simulation of delamination growth in multidirectional laminates under mode I and mixed mode I/II loadings using cohesive elements", Compos. Struct., 116(1), 509-522. https://doi.org/10.1016/j.compstruct.2014.05.042