Abstract
The energy expended during controlled crack propagation in unidirectionally reinforced composites of carbon fibre in a brittle resin matrix has been evaluated in terms of the energy dissipated during fibre-snapping, matrix-cracking and fibre pull-out. The work of fracture, γ F, is found to depend principally on the frictional shear stress at the fibre/resin interface opposing pulling out of broken fibres. Differences in γ F for carbon fibre/resin composites exhibiting a range of interfacial shear strengths and void contents have been explained with reference to variations in fracture surface topography of the fibrous composites. The effect of environment on properties of the interface and work of fracture was also investigated. The energy required to propagate a crack has been compared with the energy for fracture initiation, γ I, using a linear elastic fracture mechanics approach. It was found that fibre pull-out energy is the principal contribution to γ F, and γ I is similar to the elastic strain energy release rate at the initiation of fracture of a brittle, orthotropic solid. For crack propagation parallel to fibres, γ F and γ I are similar and not unlike the fracture surface energy of the resin alone. The strength of the interface is important only in so far as it affects the value of γ I.
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References
A. A. Griffith, Phil. Trans. Roy. Soc. A221 (1921) 163.
P. W. R. Beaumont and D. C. Phillips, J. Mater. Sci. 7 (1972) 682.
B. Harris, P. W. R. Beaumont, and E. Moncunill De Ferran, ibid 6 (1971) 238.
J. Fitzrandolph, D. C. Phillips, P. W. R. Beaumont, and A. S. Tetelman, ibid 7 (1972) 289.
J. O. Outwater and M. C. Murphy, 24th Annual Conference of Reinforced Plastics/Composites Division of Soc. Plastics Ind., paper 11-C (1969).
A. H. Cottrell, Proc. Roy. Soc. A282 (1964) 2.
G. C. Sih, P. C. Paris, and G. R. Irwin, Internat. J. Fracture Mech. 1 (1965) 189.
E. M. Wu, J. Applied Mech. Trans. ASME, Series E, 34 (1967) 967.
G. R. Irwin, “Handbuch der Physik”, 6 (Springer-Verlag, Berlin, 1958) 551.
S. W. Tsai, “Formulas for the Elastic Properties of Fiber Reinforced Composites”, Monsanto/Washington University ONR/ARPA Association, HPC 68-61 (1968).
P. W. R. Beaumont, “Fracture and Fatigue of Carbon Fibre Reinforced Plastics”, D.Phil. Thesis, School of Applied Sciences, University of Sussex (1971).
M. Isida, unpublished data described by W. F. Brown and J. E. Srawley, “Plane Strain Crack Toughness Testing of High Strength Metallic Materials”, ASTM, STP 410, 1966 p. 11.
H. G. Tattersall and G. Tappin, J. Mater. Sci. 1 (1966) 296.
B. Gross and J. E. Srawley, Technical Note D-3092, NASA, December, 1965. (Described in ASTM STP 410 p. 13.)
L. B. Greszczuk, “Effect of Voids on Strength Properties of Filamentary Composites”, Conference of Reinforced Plastics/Composites Division of SPI, 1967.
B. Budiansky, J. Mech. Phys. Solids 13 (1965) 223.
R. L. Foye, AIAA paper no. 66-143, (1966).
N. A. Weil, “Parametric Effects on the Mechanics of Ceramic Materials”, Symp. on Ceramic Materials (1966).
B. W. Rosen, AIAA J. 2 (1964) 1985.
R. C. Wyatt and K. H. G. Ashbee, Fibre Sci. and Tech. 2 (1969) 29.
P. W. R. Beaumont and B. Harris, “Effect of the Fibre-Matrix Interface on the Fracture Toughness of Carbon Fibre Resin Composites”, Fifth Symposium on Advanced Composites, St. Louis, Missouri, Washington University/Monsanto (April 1971).
R. G. C. Arridge, Nature 223 (1969) 941.
J. M. Lifshitz and A. Rotem, Fibre Sci. and Tech. 3 (1970) 1.
A. Kelly and G. J. Davies, Met. Rev. 10 (1965) 1.
B. Harris, P. W. R. Beaumont, and A. Rosen, J. Mater. Sci. 4 (1969) 432.
P. Hancock and R. C. Cuthbertson, ibid 5 (1970) 762.
P. W. R. Beaumont and D. C. Phillips, J. Comp. Mater. 6 (1972) 32.
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Beaumont, P.W.R., Harris, B. The energy of crack propagation in carbon fibre-reinforced resin systems. J Mater Sci 7, 1265–1279 (1972). https://doi.org/10.1007/BF00550692
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DOI: https://doi.org/10.1007/BF00550692