C. Soutis/Progress in Aerospace Sciences 41(2005)143-1 [19 Kashtalyan M, Soutis C. Analysis of local delaminations [25 Soutis C, Hu Fz. Failure analysis of scarf-patch-repairee nduced by angle ply matrix cracks. Int J Solids Struct omposite laminates loaded in compression. AIAA J 002;39(6:1515-37 2000:38(4):73440 [0Kashtalyan M, Soutis C. Mechanisms of internal [26 Hu FZ, Soutis C. Strength prediction of patch repaired damage and their effect on the behaviour and pr CFRP laminates loaded in Compression. J Compos Sci f cross ply laminates. Int Appl Mechan 2002: 38 (6) Technol 2000: 6 03-14. 641-57 21 Gutowski TG. Advanced composites manufacturing. New evaluation of fibre York: Wiley: 1997. [22 Soutis C, Curtis PT. Prediction of the post-impact 2y2.ency Lamb waves. J Acc Soc Am 2002: 111(5): 2026-33 iamanti K. Soutis C. Hodgkinson JM. Lamb waves for impressive strength of CFRP laminated composites the non-destructive inspection of monolithic and sandwich omp Sci Technol 1996: 56(6): 677-84 beams. Composites A 2005: 36(2): 189-95. 223 Curtis PT. Hawyes VJ, Soutis C. Effect of impact damage [29 Lavoie JA, Soutis C, Morton J. Apparent strength scaling impressive respo of in continuous fiber composite laminates. J Comp Sci opposites Part A 2001: 32(9): 1263-70 Technol20006002):283-99 224 Soutis C, Spearing SM. Compressive response of notched [30] Lee J, Soutis C. Thickness effect on the compressive oven fabric face-sheet honeycomb sandwich panels. J strength of T800/924C carbon fibre-epoxy laminates Polym Rubbers Composites 2002: 31(9): 392-7 Composites A2005:36(2):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