Composite Materials Research Progress

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234 W. Van Paepegem, I. De Baere, E. Lamkanfi et al. [9] Doyle, C., Martin, A., Liu, T., Wu, M., Hayes, S., Crosby, P.A., Powell, G.R., Brooks, D. and Fernando, G.F. (1998). In-situ process and condition monitoring of advanced fibre-reinforced composite materials using optical fibre sensors. Smart Materials & Structures, 7(2), 145-158 APR 1998. [10] De Baere, I., Voet, E., Van Paepegem, W., Vlekken, J., Cnudde, V., Masschaele, B. and Degrieck, J. (2007). Strain monitoring in thermoplastic composites with optical fibre sensors: embedding process, visualization with micro-tomography and fatigue results. Journal of Thermoplastic Composite Materials, 20 (September 2007), 453-472. [11] De Baere, I., Voet, E., Luyckx, G., Van Paepegem, W., Vlekken, J., Cnudde, V., Masschaele, B. and Degrieck, J. (2007). On the feasibility of optical fibre sensors for strain monitoring in thermoplastic composites under fatigue loading conditions. Proceedings of the Third international workshop on Optical Measurement Techniques for Structures and Systems (OPTIMESS 2007), May 28-30, 2007, Leuven, Belgium. [12] Abry, J.C., Bochard, S., Chateauminois, A., Salvia, M. and Giraud, G. (1999). In situ detection of damage in CFRP laminates by electrical resistance measurements. Composites Science and Technology, 59, 925-935. [13] Angelidis, N., Wei, C.Y. and Irving, P.E. (2004). The electrical resistance response of continuous carbon fibre composite laminates to mechanical strain. Composites Part A, 35, 1135–47. [14] Chung, D.D.L. and Wang, S. (2006). Discussion on paper ‘The electrical resistance response of continuous carbon fibre composite laminates to mechanical strain’ by Angelidis N, Wei CY, Irving PE, Composites: Part A 2004;35:1135–47. Composites Part A, 37, 1490–1494. [15] Angelidis, N., Wei, C.Y. and Irving, P.E. (2006). Short communication - Response to discussion of paper: The electrical resistance response of continuous carbon fibre composite laminates to mechanical strain. Composites Part A, 37, 1495–1499. [16] De Baere, I., Van Paepegem, W. and Degrieck, J. (2007). The use of rivets for electrical resistance measurement on carbon fibre-reinforced thermoplastics. Smart Materials and Structures, 16(5), 1821-1828. [17] De Baere, I., Van Paepegem, W. and Degrieck, J. (2007). Electrical resistance measurement on carbon fibre-reinforced thermoplastics with rivets as electrodes. Proceedings of the Fourth International Conference Emerging Techonologies in Non- Destructive Testing (ETNDT 4), Stuttgart, Germany, 2 – 4 april 2007. [18] Fujii, T., Amijima, S. and Okubo, K. (1993). Microscopic fatigue processes in a plainweave glass-fibre composite. Composites Science and Technology, 49, 327-333. [19] Schulte, K., Reese, E. and Chou, T.-W. (1987). Fatigue behaviour and damage development in woven fabric and hybrid fabric composites. In : Matthews, F.L., Buskell, N.C.R., Hodgkinson, J.M. and Morton, J. (eds.). Sixth International Conference on Composite Materials (ICCM-VI) & Second European Conference on Composite Materials (ECCM-II) : Volume 4. Proceedings, 20-24 July 1987, London, UK, Elsevier, pp. 4.89-4.99. [20] Hansen, U. (1997). Damage development in woven fabric composites during tensiontension fatigue. In : Andersen, S.I., Brøndsted, P., Lilholt, H., Lystrup, Aa., Rheinländer, J.T., Sørensen, B.F. and Toftegaard, H. (eds.). Polymeric Composites - Expanding the Limits. Proceedings of the 18th Risø International Symposium on Materials Science, 1-5 September 1997, Roskilde, Denmark, Risø International Laboratory, pp. 345-351.
Research Directions in the Fatigue Testing of Polymer Composites 235 [21] Ferry, L., Gabory, D., Sicot, N., Berard, J.Y., Perreux, D. and Varchon, D. (1997). Experimental study of glass-epoxy composite bars loaded in combined bending and torsion loads. Fatigue and characterisation of the damage growth. In : Degallaix, S., Bathias, C. and Fougères, R. (eds.). International Conference on fatigue of composites. Proceedings, 3-5 June 1997, Paris, France, La Société Française de Métallurgie et de Matériaux, pp. 266-273. [22] Herrington, P.D. and Doucet, A.B. (1992). Progression of bending fatigue damage around a discontinuity in glass/epoxy composites. Journal of Composite Materials, 26(14), 2045-2059. [23] Chen, A.S. and Matthews, F.L. (1993). Biaxial flexural fatigue of composite plates. In : Miravete, A. (ed.). ICCM/9 Composites : properties and applications. Volume VI. Proceedings of the Ninth International Conference on Composite Materials, 12-16 July 1993, Madrid, Spain, Woodhead Publishing Limited, pp. 899-906. [24] Sidoroff, F. and Subagio, B. (1987). Fatigue damage modelling of composite materials from bending tests. In : Matthews, F.L., Buskell, N.C.R., Hodgkinson, J.M. and Morton, J. (eds.). Sixth International Conference on Composite Materials (ICCM-VI) & Second European Conference on Composite Materials (ECCM-II) : Volume 4. Proceedings, 20- 24 July 1987, London, UK, Elsevier, pp. 4.32-4.39. [25] El Mahi, A., Berthelot, J.-M. and Bezazi, A. (2002). The fatigue behaviour and damage development in cross-ply laminates in flexural tests. Proceedings of the Tenth European Conference on Composite Materials (ECCM-10), Brugge, Belgium, 3-7 June 2002. [26] Caprino, G. and D'Amore, A. (1998). Flexural fatigue behaviour of random continuousfibre-reinforced thermoplastic composites. Composites Science and Technology, 58, 957-965. [27] Van Paepegem, W. and Degrieck, J. (2002). A New Coupled Approach of Residual Stiffness and Strength for Fatigue of Fibre-reinforced Composites. International Journal of Fatigue, 24(7), 747-762. [28] Van Paepegem, W. and Degrieck, J. (2001). Fatigue Degradation Modelling of Plain Woven Glass/epoxy Composites. Composites Part A, 32(10), 1433-1441. [29] Van Paepegem, W. and Degrieck, J. (2002). Modelling damage and permanent strain in fibre-reinforced composites under in-plane fatigue loading. Composites Science and Technology, 63(5), 677-694. [30] Van Paepegem, W. and Degrieck, J. (2005). Simulating Damage and Permanent Strain in Composites under In-plane Fatigue Loading. Computers & Structures, 83(23-24), 1930-1942. [31] Lessard, L.B., Eilers, O.P. and Shokrieh, M.M. (1995). Testing of in-plane shear properties under fatigue loading. Journal of Reinforced Plastics and Composites, 14, 965-987. [32] Van Paepegem, W., De Baere, I. and Degrieck, J. (2006). Modelling the nonlinear shear stress-strain response of glass fibre-reinforced composites. Part I: Experimental results. Composites Science and Technology, 66(10), 1455-1464. [33] Van Paepegem, W., De Baere, I. and Degrieck, J. (2006). Modelling the nonlinear shear stress-strain response of glass fibre-reinforced composites. Part II: Model development and finite element simulations. Composites Science and Technology , 66(10), 1465- 1478.
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COMPOSITE MATERIALS RESEARCH PROGRE
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Copyright © 2008 by Nova Science P
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vi Contents Chapter 9 Recent Advanc
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viii Lucas P. Durand scale transiti
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x Lucas P. Durand machine. In paral
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In: Composite Materials Research Pr
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Multi-scale Analysis of Fiber-Reinf
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T300 fibers (Soden et al., 1998; Ag
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1 I L = L : r v Multi-scale Analysi
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I E ⎡0 ⎢ ⎢0 ⎢ ⎢ ⎢ ⎢0
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Applied macroscopic load Correspond
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In: Composite Materials Research Pr
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Optimization of Laminated Composite
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⎧σ x ⎫ ⎡ mE ⎪ ⎪ ⎢ x
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and γ 2 γ 0 Optimization of Lamin
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4 x 10 5 4 3 2 1 Compliance (Nmm) 0
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3.5 3 2.5 2 1.5 1 Optimization of L
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110 W.H. Zhong, R.G. Maguire, S.S.
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112 Reinforcement: Advanced materia
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130 Yuanxin Zhou, Hassan Mahfuz, Vi
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140 Heat Flow (W/g) Heat Flow (W/g)
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144 Material Yuanxin Zhou, Hassan M
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146 SEM Analysis Yuanxin Zhou, Hass
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150 Governing Equation For the fibe
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152 ⎧ UU = ⎨ ⎩ ⎧ UD = ⎨
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156 Stress (MPa) 120 80 40 0 Yuanxi
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166 Giangiacomo Minak and Andrea Zu
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170 ⎟ ⎞ ⎠ s ⎜ ⎛ ⎝ = a E
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Page 198 and 199: 184 Giangiacomo Minak and Andrea Zu
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Page 204 and 205: 190 D D 1.0 0.9 0.8 0.7 0.6 0.5 0.4
Page 218 and 219: 204 Conclusion Giangiacomo Minak an
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Page 225 and 226: Research Directions in the Fatigue
Page 241 and 242: Bending force [N] Research Directio
Page 247: Research Directions in the Fatigue
Page 253 and 254: Damage Variables in Impact Testing
Page 263 and 264: F peak [kN] 16 14 12 10 8 6 4 2 0 D
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284 S.C. Tjong where DL is lattice
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286 S.C. Tjong stress is temperatur
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288 S.C. Tjong threshold stress res
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290 S.C. Tjong NC Al, and the NC Al
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292 S.C. Tjong (a) (b) Figure 19. T
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294 S.C. Tjong Apart from forming u
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296 S.C. Tjong [29] Saravanan, M.;
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298 braids, 115 broadband, 211 bubb
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300 endothermic, 139 endurance, 32
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302 isostatic pressing, 279, 288 It
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304 piezoelectricity, 261 pitch, 12
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306 67, 69, 70, 71, 72, 73, 84, 94,
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