Modelling damage evolution in composite laminates subjected to low velocity impact

Composite Structures - Tập 94 Số 9 - Trang 2902-2913 - 2012
Yu Shi1, T.J. Swait1, C. Soutis1
1Department of Mechanical Engineering (Aerospace), The University of Sheffield, Mappin Street, Sheffield, S1 3JD, UK

Tóm tắt

Từ khóa


Tài liệu tham khảo

Abrate, 1998

Davies, 2004, Impact on composite structures, Aeronaut J, 108, 541, 10.1017/S0001924000000385

Matthews, 2000

Donadon, 2008, A progressive failure model for composite laminates subjected to low velocity impact damage, Comput Struct, 86, 1232, 10.1016/j.compstruc.2007.11.004

Faggiani, 2010, Predicting low-velocity impact damage on a stiffened composite panel, Composites Part A, 41, 737, 10.1016/j.compositesa.2010.02.005

Iannucci, 2006, An energy based damage model for thin laminated composites, Compos Sci Technol, 66, 934, 10.1016/j.compscitech.2005.07.033

Yokoyama, 2010, A numerical study on the impact resistance of composite shells using an energy based failure model, Compos Struct, 93, 142, 10.1016/j.compstruct.2010.06.006

Kachanov, 1958, On the creep rupture time, Izv AN SSSR Otd Tekhn Nauk, 8, 26

Rabotnov, 1963

Kashtalyan, 2000, The effect of delaminations induced by transverse cracks and splits on stiffness properties of composite laminates, Composites Part A, 31, 107, 10.1016/S1359-835X(99)00066-4

Kashtalyan, 2002, Analysis of local delaminations in composite laminates with angle-ply matrix cracks, Int J Solid Struct, 39, 1515, 10.1016/S0020-7683(02)00007-0

Zhang, 1992, Analysis of multiple matrix cracking in [±θm/90n]s composite laminates. Part 1: in-plane stiffness properties, Composites, 23, 291, 10.1016/0010-4361(92)90327-Q

Berbinau, 1999, Effect of off-axis ply orientation on 0°-fibre microbuckling, Composites Part A, 30, 1197, 10.1016/S1359-835X(99)00026-3

Berbinau, 1999, Compressive failure of 0° unidirectional carbon-fibre-reinforced plastic (CFRP) laminates by fibre micobuckling, Compos Sci Technol, 59, 1451, 10.1016/S0266-3538(98)00181-X

Diaz Valdes, 2000, Health monitoring of composites using lamb waves generated by piezo-electric devices, Plast Rubber Compos, 29, 496, 10.1179/146580100101541328

Diaz Valdes, 2002, Real-time non-destructive evaluation of fibre composite laminates using low-frequency lamb waves, J Acc Soc Am, 111, 2026, 10.1121/1.1466870

Anderson, 1995

Kashtallyan, 2002, Mechanisms of internal damage and their effect on the behaviour and properties of cross-ply composite laminates, Int Appl Mech, 38, 641, 10.1023/A:1020456726805

Zhang, 1994, Strain energy release rate associated with local delamination in cracked composite laminates, Composites, 25, 851, 10.1016/0010-4361(94)90026-4

Tita, 2008, Failure analysis of low velocity impact on thin composite laminates: experimental and numerical approaches, Compos Struct, 83, 413, 10.1016/j.compstruct.2007.06.003

Hashin, 1973, A fatigue failure criterion for fiber-reinforced materials, J Compos Mater, 7, 448, 10.1177/002199837300700404

Hashin, 1980, Failure criteria for uni-directional fibre composites, J Appl Mech, 47, 329, 10.1115/1.3153664

Puck, 1998, Failure analysis of FRP laminates by means of physically based phenomenological models, Compos Sci Technol, 58, 1045, 10.1016/S0266-3538(96)00140-6

Bažant, 1983, Crack band theory for fracture of concrete, Mater Struct, 16, 155

Lapczyk, 2007, Progressive damage modelling in fiber-reinforced materials, Composites Part A, 38, 2333, 10.1016/j.compositesa.2007.01.017

Camanho PP, Dávila CG. Mixed-Mode decohesion finite elements for the simulation of delamination in composite materials. Tech Rep NASA/TM-2002-211737; 2002.

ABAQUS. ABAQUS Version 6.10, Dessault systemes. Providence, RI; 2010.

Khan, 1995

Lemaitre, 1990

Danesi, 1996, Coupled plastic-damaged model, Comput Method Appl Mech Eng, 129, 81

ASTM D7136/D7136M-07. Standard test method for measuring the damage resistance of a fibre-reinforced polymer matrix composite to a drop-weight impact event. Philadelphia: American Society for Testing and Materials; 2007.

Jumahat, 2011, A graphical method predicting the compressive strength of toughened unidirectional composite laminates, Appl Compos Mater, 18, 65, 10.1007/s10443-010-9149-8

Chang, 1995, An accumulative damage model for tensile and shear failures of laminated composite plates, J Compos Mater, 29, 926, 10.1177/002199839502900705

Pinho, 2006, Fracture toughness of the tensile and compressive fibre failure modes in laminated composites, Compos Sci Technol, 66, 22069, 10.1016/j.compscitech.2005.12.023

Sung, 1979, Effect of fiber orientation on friction and wear of fiber reinforced polymeric composites, Wear, 53, 129, 10.1016/0043-1648(79)90224-2

Schon, 2000, Coefficient of friction of composite delamination surfaces, Wear, 237, 77, 10.1016/S0043-1648(99)00315-4

Bing Q, Sun CT. Effect of transverse normal stress on mode II fracture toughness in fiber composites. In: 16th International conference on composite materials, Kyoto, Japan; 2007.

Soutis, 2006, Fracture of layered composites by internal fibre instability: effect of interlaminar adhesion, Aeronaut J, 110, 185, 10.1017/S0001924000001160

Soutis, 2000, Predicting the compressive engineering performance of carbon fibre-reinforced plastics, Composites Part A, 31, 531, 10.1016/S1359-835X(99)00103-7

Lavoie, 2000, Apparent strength scaling in continuous fiber composite laminates, Compos Sci Technol, 60, 283, 10.1016/S0266-3538(99)00124-4

Lee, 2007, A study on the compressive strength of thick carbon fibre/epoxy laminates, Compos Sci Technol, 67, 2015, 10.1016/j.compscitech.2006.12.001

Curtis, 2001, Effect of impact damage on the compressive response of composite laminates, Composites Part A, 32, 1263, 10.1016/S1359-835X(01)00072-0

Soutis, 1996, Prediction of the post-impact compressive strength of CFRP laminated composites, Compos Sci Technol, 56, 677, 10.1016/0266-3538(96)00050-4