Composite Materials Research Progress

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206 Giangiacomo Minak and Andrea Zucchelli [28] Found MS, Lamb JR, Damage assessment of impacted thin CFRP panels, Composite: Part A, 35(9), (2004) 1039–1047 [29] Luo RK, Green ER, Morrison CJ, Impact damage analysis of composite plates, International Journal of Impact Engineering, 22 , (1999) 435-447 [30] Caprino G, Teti R. Residual strength evaluation of impacted GRP laminates with acoustic emission monitoring, Composites Science and Technology, 53, (1995) 13-19 [31] Cartié DDR, Irving PE. Effect of Resin and Fibre Properties of Impact and Compression after Impact Performances of CFRP, Composites Part A, 33 (4), (2002) 483-493 [32] Zhang X, Davies GAO, Hitchings D, Impact damage with compressive preload and post-impact compression of carbon composite plates, International Journal of Impact Engineering, 22 , (1999) 485-509 [33] Caprino G, Residual strength prediction of impacted CFRP laminates, Journal of Composite Materials,18, (1984) 508-518. [34] Caprino G, Teti R, de Iorio I, Predicting residual strength of pre-fatigued glass fibrereinforced plastic laminates through acoustic emission monitoring, Composites Part B, 36 (2005) 365-371 [35] Cesari F, Dal Re V, Minak G, Zucchelli A, Damage and residual strength of laminated graphite-epoxy composite circular plates loaded at the centre, Composites Part A, 38 (2007), 1163-1173 [36] Symons DD, Davis G, Fatigue testing of impact-damage T300/914 carbon-fibrereinforced plastic, Composite Science and Technology, 60(3), 2000, 379-389 [37] Minak G, Morelli P, Zucchelli A, Fatigue residual strength of laminated graphite-epoxy circular plates damaged by transversal load, Proceedings of the 12 th European Conference on Composite Materials, Biarritz, (2006) [38] Dunegan HL, Harris DO, Tatro CA, Fracture analysis by use of acoustic emission Engineering Fracture Mechanics, 1 (1), (1968) 105-110 [39] Shippen NC, Adams DF, Acoustic Emission monitoring of damage progression in graphite/epoxy laminates, Journal of Reinforced Plastics and Composites, 4(1985) 242-261 [40] Siron O, Tsuda H, Acoustic Emission in Carbon Fibre-Reinforced Plastics Materials, Annales De Chimie et Science des Matériaux, 25, 7, (2000) 533-537, [41] Mizutani Y, Nagashima K, Takemoto M, Ono K, Fracture mechanism characterization of cross-ply carbon-fibre composites using acoustic emission analysis, NDT&E International, 33 (2000) 101-110 [42] Walker JL, Hill E, Workman GL, Russell SS, A Neural Network-Acoustic Emission Analysis of Impact Damaged Graphite-Epoxy Pressure Vessels, Proceedings of the ASNT 1995 Spring Conference, Las Vegas (1995) 106–108. [43] Prosser WH, Waveform Analysis of AE from Composites. Proceedings of the Sixth International Symposium on Acoustic Emission from Composite Materials (AECM-6), San Antonio (1998) 61–70. [44] Prosser WH, Jackson KE, Kellas S, Smith BT, McKeon J, Friedman A, Advanced, Waveform Based Acoustic Emission Detection of Matrix Cracking in Composites. Materials Evaluation 53(9),(1995) 1052–1058 [45] Woo SC, Choi NS, Analysis of fracture process in single-edge-notched laminated composites based on the high amplitude acoustic emission events, Composites Science and Technology, 67 (2007) 1451-1458
Damage Evaluation and Residual Strength Prediction of CFRP Laminates … 207 [46] Shull PJ, Non destructive Evaluation: Theory, Techniques, and Applications, Marcel Dekker Inc., 2002. [47] Zucchelli A, Dal Re V, Experimental analysis of composite laminate progressive failure by AE monitoring, Proceedings ICEM12 - 12th International Conference on Experimental Mechanics, Bari (2004) [48] MIL-HDBK-17-3E; Department of Defence Handbook, Polymer Matrix Composites, volume 3. Materials Usage, Design, and Analysis. [49] Shim VPW, Yang LM, Characterization of the residual mechanical properties of woven fabric reinforced composites after low-velocity impact, International Journal of Mechanical Sciences, 47, 2005, 647-665 [50] Caprino G, Lopresto V, The significance of indentation in the inspection of carbon fibre-reinforced plastic panels damaged by low velocity impact, Composites Science and Technology, 60, (2000) 1003-1012 [51] Sanchez-Saez S, Barbero E, Zaera R, Navarro E., Compression after impact of thin composite laminates, Composites Science and Technology, 65, (2005) 1911-1919 [52] Qi B, Herszberg I, An engineering approach for predicting residual strength of carbon/epoxy laminates after impact and hygro-thermal cycling, Composite Structures, 47, (1999) 483-490
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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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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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Page 170 and 171: 156 Stress (MPa) 120 80 40 0 Yuanxi
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Page 180 and 181: 166 Giangiacomo Minak and Andrea Zu
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Page 202 and 203: 188 A B E (MPa) D 250000 200000 150
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
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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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Eletromechanical Field Concentratio
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MV/m. Eletromechanical Field Concen
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276 S.C. Tjong developed in the pas
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278 S.C. Tjong ultrasonic waves gen
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280 S.C. Tjong applications. Goujon
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282 S.C. Tjong nanoparticles were p
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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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