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C Soutis/Progress in Aerospace Sciences 41(2005)143-151 151 [2 [22]Soutis C 1996566677 2005362:189-95 on the Polym Rubbers Composites 2002:31937. C0m8A20s-362,213-27. [19] Kashtalyan M, Soutis C. Analysis of local delaminations induced by angle ply matrix cracks. Int J Solids Struct 2002;39(6):1515–37. [20] Kashtalyan M, Soutis C. Mechanisms of internal damage and their effect on the behaviour and properties of cross-ply laminates. Int Appl Mechan 2002;38(6): 641–57. [21] Gutowski TG. Advanced composites manufacturing. New York: Wiley; 1997. [22] Soutis C, Curtis PT. Prediction of the post-impact compressive strengthof CFRP laminated composites. Comp Sci Technol 1996;56(6):677–84. [23] Curtis PT, Hawyes VJ, Soutis C. Effect of impact damage on the compressive response of composite laminates. Composites Part A 2001;32(9):1263–70. [24] Soutis C, Spearing SM. Compressive response of notched woven fabric face-sheet honeycomb sandwich panels. J Polym Rubbers Composites 2002;31(9):392–7. [25] Soutis C, Hu FZ. Failure analysis of scarf-patch-repaired composite laminates loaded in compression. AIAA J 2000;38(4):734–40. [26] Hu FZ, Soutis C. Strengthprediction of patchrepaired CFRP laminates loaded in Compression. J Compos Sci Technol 2000;60(7):1103–14. [27] Diaz Valdes SH, Soutis C. Real-time non-destructive evaluation of fibre composite laminates using low-fre￾quency Lamb waves. J Acc Soc Am 2002;111(5):2026–33. [28] Diamanti K, Soutis C, Hodgkinson JM. Lamb waves for the non-destructive inspection of monolithic and sandwich composite beams. Composites A 2005;36(2):189–95. [29] Lavoie JA, Soutis C, Morton J. Apparent strengthscaling in continuous fiber composite laminates. J Comp Sci Technol 2000;60(2):283–99. [30] Lee J, Soutis C. Thickness effect on the compressive strengthof T800/924C carbon fibre-epoxy laminates. Composites A 2005;36(2):213–27. ARTICLE IN PRESS C. Soutis / Progress in Aerospace Sciences 41 (2005) 143–151 151
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