Abstract
In order to etablish DCB as a general quantitative method, an advanced understanding on this configuration is necessary. Using different angle ply laminates of glass/epoxy, we have tried to explain the effect of lay-up of laminates upon the pure mode I critical energy release rate. The results obtained revealed that in the multidirectional DCB specimen, three dimentional effects are too strong to be negnected. Application of the compliance method requires a more exact theoretical analysis. GIc measured in this study seems indenpendent of specimen rigidity, but varies with curvature couplings ky/kx and kxy/kx.
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References
De Charentenay F.X., Harry J.M., Prel Y. and Benzeggagh M.L., Effect of defects in composite material, ASTM.STP 836 (1980) pp.84–103
Benzeggagh M.L., Prel Y. and De Charentenay EX., Fifth International Conference on Composite Materials, ICCM-V (1985.) pp. 127–139
Hwang W. and Han K.S.,Journal of Composite Materials, 23(April 1989) pp.386–431
Hu M.Z., Kolsky H. and Pipkin A.C., J. Comp. Mat., 19 (May 1985) pp.235–249
Aliyuand A.A., Daniel I.M., ASTM.STP 876 (1985) pp.236–248
Hunston D.L. and Bascom W.D., Comp. Tech. Reviex (1983) pp.118–119
Kageyama K., Kobayashi T. and Chou T.W., Composites, 18, n° 5 (Novembre 1987) pp.393–399
MohamadS., El-Zein and Kenneth, Reifsnider L., Journal of Composites Technology & Research, 10, n° 4 (Winter 1988) pp.151–155
Wang A.S.D., Composites Technology Review, 6, n° 2 (Summer 1984) pp.45–62
El Senussi A.K. and Webber J.P.H., Composites, 20, n° 3 (May 1989) pp.249–259
Marom G., Romain I, Harrel H. and Rosensatt M., ICCM-VI, 3, pp.65–273
Miller A.G., Hertzberg P.E., and Rantala V.W., 12th Nationale SAMPE Technical Conference (Octobre 7–9 1980) pp. 279–293
Wilkins D.J., Eisenmann J.R., Camin R.A., Margolis W.S. and Benson R.A., ASTM. STP 775 (1982) 168–183
Jordan W.M. and Bradley W.L., ASTM.STP 937 (1985)
Nicholls D.J. Gallagher J.P., J. of Reinforced Plastics and Composites, 2 (January 1983) pp.2–17
Chai H., Composites, 15, n° 4 (Octobre 1984) pp.277–290
Ramkumar R.L. and Whitcomb J.D., ASTM.STP 876 (1985) pp.315–335
Johnson W.S. and Mangalgiri P.D., Nasa Technical Memorandum 87716 (Avril 1986)
Benzeggagh M.L., Gong X.J., Roelandt J.M., ICCM-VII (1989) pp.210–216
Davidson B.D.and Schapery R.A.,J.of Comp. Mate., 22(July1988), pp.640–656
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© 1990 Elsevier Science Publishers Ltd
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Gong, X.J., Benzeggagh, M., Laksimi, A., Roelandt, J.M. (1990). Characterizing Pure Mode I Delamination Using Multidirectional DCB Specimens for Glass/Epoxy. In: Füller, J., Grüninger, G., Schulte, K., Bunsell, A.R., Massiah, A. (eds) Developments in the Science and Technology of Composite Materials. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-0787-4_20
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DOI: https://doi.org/10.1007/978-94-009-0787-4_20
Publisher Name: Springer, Dordrecht
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