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Mechanical Behavior of Mode I Delamination of a Laminated Composite Material

Year 2019, Volume: 7 , 68 - 75, 24.11.2019

Abstract

The objective of our work is to analyze numerically in three dimensions by the finite element method of the effect of a mechanical load on the delamination of unidirectional and multidirectional stratified composites in order to determine the energy release rate G in Mode I and the Von Mises equivalent stress distribution along the damaged area under the influence of several parameters such as applied load and delamination size. The results obtained in this study show that unidirectional composite laminates have better mechanical strength on the loading line than multi-directional composite laminates.

References

  • Bai, T. and Pollard, D.D. 1999, “Spacing of fractures in a multilayerat fracture saturation”,International Journal of Fracture, 100(4),pp. 23–24. Berthelot, J.-M. and Le Corre, J.-F. 2000, “Statistical analysis of the progression of transverse cracking and delamination in cross-ply laminates”, Composites Science and Technology, 60(3), pp. 2659–2669. Haneef, M., R M S. A. & 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 6 - 8, London, U.K.. Katerelos, D.T.G., Kashtalyan, M., Soutis, C. and Galiotis, C. 2008, “Matrix cracking in polymeric composites laminates Modeling and experiments”,Composites Science and Technology, pp. 2310-2317. 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 Sci18, pp. 2876-2889. Product DassaultSystèmesSimuliaCorp2010, ABAQUS Standard Version 6.10, Providence, RI, USA.. Qing n, 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 Elements in Analysis and Design, 47, pp. 1017–1024. Rebière, J.-L, Maâtallah, M.-N and Gamby, D. 2002, “Analysis of damage mode transition in a cross-ply laminate under uniaxial loading”, Composites structures, 55,pp. 115-126. Smith B. W. 1993, “Fractography for continuous fiber composites”, in "Engineered materials handbook", volume 1: composite, Ohio, USA, ASM International, pp: 786-793, ISBN 0871702797 (v.1). Dasa, Subhankar, Choudhurya, Pannalal, Haldera, Sudipta and Sriramb, P. 2013 “Stress and free edge delamination analyses of delaminated composite structure using ANSYS”, Procedia Engineering, , 64 1364 – 1373 Szekrényes, András, 2012 “Interlaminar stresses and energy release rates in delaminated orthotropic composite plates. International Journal of Solids and Structures, 49 2460–2470. Todo, M., JAR, P. Y. B. and Takahashi, K. 2000, “Initiation of a Mode-II Interlaminar Crack from an Insert Film in End-Notched Flexure Composite Specimen”, Composites Science and Technology, 60, pp. 263–272. Todo, M.,Jar, P. Y. B. 1998, “Study of Mode-I Interlaminar Crack Growth in DCB Specimens ofFibre-Reinforced Composites”, Composites Science and Technology, 58, pp. 105–118. Wang, J. and Karihaloo, B. L. 1997, “Matrix crack-induced delamination in composite laminates under transverse loading”, Composites structures, 38, 661-666. Yao, Liaojun, Alderliesten, R.C., Zhao, Meiying and Benedictus, R. 2014, “Discussion on the use of the strain energy release rate for fatigue delamination characterization”.Composites: Part A, 66 65–72.
Year 2019, Volume: 7 , 68 - 75, 24.11.2019

Abstract

References

  • Bai, T. and Pollard, D.D. 1999, “Spacing of fractures in a multilayerat fracture saturation”,International Journal of Fracture, 100(4),pp. 23–24. Berthelot, J.-M. and Le Corre, J.-F. 2000, “Statistical analysis of the progression of transverse cracking and delamination in cross-ply laminates”, Composites Science and Technology, 60(3), pp. 2659–2669. Haneef, M., R M S. A. & 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 6 - 8, London, U.K.. Katerelos, D.T.G., Kashtalyan, M., Soutis, C. and Galiotis, C. 2008, “Matrix cracking in polymeric composites laminates Modeling and experiments”,Composites Science and Technology, pp. 2310-2317. 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 Sci18, pp. 2876-2889. Product DassaultSystèmesSimuliaCorp2010, ABAQUS Standard Version 6.10, Providence, RI, USA.. Qing n, 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 Elements in Analysis and Design, 47, pp. 1017–1024. Rebière, J.-L, Maâtallah, M.-N and Gamby, D. 2002, “Analysis of damage mode transition in a cross-ply laminate under uniaxial loading”, Composites structures, 55,pp. 115-126. Smith B. W. 1993, “Fractography for continuous fiber composites”, in "Engineered materials handbook", volume 1: composite, Ohio, USA, ASM International, pp: 786-793, ISBN 0871702797 (v.1). Dasa, Subhankar, Choudhurya, Pannalal, Haldera, Sudipta and Sriramb, P. 2013 “Stress and free edge delamination analyses of delaminated composite structure using ANSYS”, Procedia Engineering, , 64 1364 – 1373 Szekrényes, András, 2012 “Interlaminar stresses and energy release rates in delaminated orthotropic composite plates. International Journal of Solids and Structures, 49 2460–2470. Todo, M., JAR, P. Y. B. and Takahashi, K. 2000, “Initiation of a Mode-II Interlaminar Crack from an Insert Film in End-Notched Flexure Composite Specimen”, Composites Science and Technology, 60, pp. 263–272. Todo, M.,Jar, P. Y. B. 1998, “Study of Mode-I Interlaminar Crack Growth in DCB Specimens ofFibre-Reinforced Composites”, Composites Science and Technology, 58, pp. 105–118. Wang, J. and Karihaloo, B. L. 1997, “Matrix crack-induced delamination in composite laminates under transverse loading”, Composites structures, 38, 661-666. Yao, Liaojun, Alderliesten, R.C., Zhao, Meiying and Benedictus, R. 2014, “Discussion on the use of the strain energy release rate for fatigue delamination characterization”.Composites: Part A, 66 65–72.
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Details

Primary Language English
Subjects Engineering
Journal Section Articles
Authors

Habib Achache

Abdi Ghezaıl

Bouabdellah Abed

Abdelouahab Benzerdjeb

Publication Date November 24, 2019
Published in Issue Year 2019Volume: 7

Cite

APA Achache, H., Ghezaıl, A., Abed, B., Benzerdjeb, A. (2019). Mechanical Behavior of Mode I Delamination of a Laminated Composite Material. The Eurasia Proceedings of Science Technology Engineering and Mathematics, 7, 68-75.