Structural Engineering and Mechanics

  • 제55권1호
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  • Pages.191-204
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  • 2015
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  • 1225-4568(pISSN)
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  • 1598-6217(eISSN)
테크노프레스 (Techno-Press)
권호 표지
DOI QR코드

DOI QR Code

Evaluation of energy release rate of composites laminated with finite element method

  • Achache, Habib (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) ;
  • Benzerdjeb, Abdelouahab (University of Science and Technology Oran Mohammed Boudiaf (USTO)) ;
  • Ouinas, Djamel (Laboratory of Numerical and experimental modeling of mechanical phenomena, University of Mostaganem)
  • 투고 : 2014.08.04
  • 심사 : 2015.06.09
  • 발행 : 2015.07.10
⟨ 이전 논문 다음 논문 ⟩

초록

Control of the mechanical behavior of composite materials and structures under monotonic and dynamic loads for cracks and damage is a vast and complex area of research. The modeling of the different physical phenomena and behavior characteristics of a composite material during deformation play an important role in the structural design. Our study aims to analyze numerically the energy release rate parameter G of a composite laminated plate (glass or boron / epoxy) cross-ply [$+{\alpha}$, $-{\alpha}$] in the presence of a crack between two circular notches under the effect of several parameters such as fiber orientation ${\alpha}$, the crack orientation ${\beta}$, the orientation ${\gamma}$ of the two considered circular notches and the effect of mechanical properties. Our results show clearly that both notches orientation has more effect on G than the cracks and fibers orientations.

키워드

참고문헌

  1. Achache, H., Boutabout, B. and Ouinas, D. (2013), "Mechanical behavior of laminated composites with circular holes", Key Eng. Mater., 550, 1-8. https://doi.org/10.4028/www.scientific.net/KEM.550.1
  2. Bai, T. and Pollard, D.D. (1999), "Spacing of fractures in a multilayerat fracture saturation", Int. J. Fract., 100(4), 23-24. https://doi.org/10.1023/A:1018748026019
  3. Berthelot, J.M. and Le Corre, J.F. (2000), "Statistical analysis of the progression of transverse cracking and delamination in cross-ply laminates", Compos. Sci. Tech., 60(3), 2659-2669. https://doi.org/10.1016/S0266-3538(00)00140-8
  4. Bouziane, S., Bouzerd, H., Boulares, N. and Guenfoud, M. (2014) "Energy release rate for kinking crack using mixed finite element", Struct. Eng. Mech., 50(5), 665-677. https://doi.org/10.12989/sem.2014.50.5.665
  5. Das, S., Choudhury, P., Halder, S. and Sriram, P. (2013), "Stress and free edge delamination analyses of delaminated composite structure using ANSYS", Procedia Eng., 64, 1364-1373. https://doi.org/10.1016/j.proeng.2013.09.218
  6. Haneef, M., Shabbir Ahmed, R.M. 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.
  7. Katerelos, D.T.G., Kashtalyan, M., Soutis, C. and Galiotis, C. (2008), "Matrix cracking in polymeric composites laminates Modeling and experiments", Compos. Sci. Tech., 68(12), 2310-2317. https://doi.org/10.1016/j.compscitech.2007.09.013
  8. Manders, P.W., Chou, T.W., Jones, F.R. and Rock, J.W. (1983)," Statistic al analysis of multiple fracture in 0/90/0 glass fiber/epoxy laminates", J. Mater. Sci., 18, 2876-2889. https://doi.org/10.1007/BF00700768
  9. Product Dassault Systemes Simulia Corp (2010), ABAQUS Standard Version 6.10, Providence, RI, USA.
  10. Qing, G.H., Liu, Y.H. and Li, D.H. (2011), "A semi-analytical model for the energy release rate analyses of composite laminates with a delamination", Finite Elem. Anal. Des., 47, 1017-1024. https://doi.org/10.1016/j.finel.2011.03.017
  11. Rebiere, J.L, Maatallah, M.N and Gamby, D. (2002), "Analysis of damage mode transition in a cross -ply laminate under uniaxial loading", Compos. Struct., 55, 115-126. https://doi.org/10.1016/S0263-8223(01)00133-7
  12. Rice, J.R. (1968), "A path independent integral and the approximate analysis of strain concentration by notches and cracks", J. Appl. Mech., 35(2), 379-386. https://doi.org/10.1115/1.3601206
  13. Seo, D.C. and Lee, J.J. (2002), "Fatigue crack growth behavior of cracked aluminum platerepaired with composite patch", Korea, Compos. Struct., 57, 323-330. https://doi.org/10.1016/S0263-8223(02)00095-8
  14. Smith, B.W. (1993), Fractography for Continuous Fber Composites, Dans, Engineered Materials Handbook, Volume 1: Composite, Ohio, USA, ASM International.
  15. Szekrenyes, A. (2012), "Interlaminar stresses and energy release rates in delaminated orthotropic composite plates", Int. J. Solid. Struct., 49, 2460-2470. https://doi.org/10.1016/j.ijsolstr.2012.05.010
  16. Todo, M. and Jar, P.Y. (1998), "Study of mode-I interlaminar crack growth in DCB specimens of fibre-reinforced composites", Compos. Sci. Tech., 58, 105-118. https://doi.org/10.1016/S0266-3538(97)00102-4
  17. Todo, M., Jar, P.Y. and Takahashi, K. (2000), "Initiation of a mode-II interlaminar crack from an insert film in end-notched flexure composite specimen", Compos. Sci. Tech., 60, 263-272. https://doi.org/10.1016/S0266-3538(99)00119-0
  18. Wang, J. and Karihaloo, B.L. (1997), "Matrix crack-induced delamination in composite laminates under transverse loading", Compos. Struct., 38, 661-666. https://doi.org/10.1016/S0263-8223(97)00103-7
  19. Yao, L.J., Alderliesten, R.C., Zhao, M.Y. and Benedictus, R. (2014),"Discussion on the use of the strain energy release rate for fatigue delamination characterization", Compos. Part A, 66, 65-72.