Woerden H J M, Sinke J, Hooijmeijer P A. Maintenance of glare structures and glare [J]. Applied Composite Materials, 2003, 10(4/5): 307-329.
[2]
Sadighi M, Prnnen T, Alderliesten R C, Sayeaftabi M, Benedictus R. Experimental and numerical investigation of metal type and thickness effects on the impact resistance of fiber metal laminates [J]. Appl Compos Mater, 2012, 19(3/4): 545-559.
[3]
朱炜垚, 许希武. 复合材料层合板低速冲击损伤的有限元模拟[J]. 复合材料学报, 2010, 27(6): 200-207. Zhu Weiyao, Xu Xiwu. Finite element simulation of low velocity impact damage on composite laminates[J]. Acta Materiae Compositae Sinica, 2010, 27(6): 200-207.
[4]
Mccarthy C T,Mccarthy M A,Lawlor V P. Progressive damage analysis of multi-bolt composite joints with variable bolt-hole clearance [J]. Composites: Part B, 2005, 36(4): 290-305.
[5]
Maa R H, Cheng J H. A CDM-based failure model for predicting strength of notched composite laminates [J]. Composites: Part B, 2002, 33(6): 479-489.
[6]
Maim P, Camanho P P, Mayugo J A, Vila C G D. A continuum damage model for composite laminates Part Ⅰ: Constitutive model [J]. Mech Mater, 2007, 39: 897-908.
[7]
Maire J F, Chaboche J L. A new formulation of continuum damage mechanics (CDM) for composite materials [J]. Aero Sci Tech, 1997, 1(4): 247-257.
[8]
Allix O, Ladeveze P. Interlaminar surface modelling for the prediction of delamination[J]. Composite Structure, 1992, 22: 235-242.
[9]
Ladeveze P, Dantec E L. Damage modelling of the elementary ply for laminated composites [J]. Composites Science and Technology, 1992, 43: 257-267.
[10]
Phillips E A, Herakovich C T, Graham L L. Damage development in composites with large stress gradients[J]. Composite Science Technology, 2001, 61: 2169-2182.
[11]
Mccarthy M A,Xiao J R, Petrinic N, Kamoulakos A, Melito V. Modelling of bird strike on an aircraft wing leading edge made from fiber metal laminates Ⅰ : Material modelling [J]. Applied Composite Materials, 2004, 11: 295-315.
[12]
Thiruppukuzhi S V, Sun C T. Models for the strain-rate-dependent behavior of polymer composites [J]. Composites Science and Technology, 2001, 61: 1-12.
[13]
Linde P, Middendorf P, Broucke B V D, Boer H D. Numerical simulation of damage behaviour of textile reinforced composites in aircraft structures [C]//27th International Congress of the Aeronautical Sciences. Dallas: ICAS, 2010.
[14]
Laliberté J, Poon C. Numerical modelling of low velocity impact damage in fibre metal laminates [C]//23th International Congress of the Aeronautical Sciences. Tornoto, Canada: ICAS, 2002.
[15]
Xiao X. A coupled damage plasticity model for energy absorption in composite [J]. International Journal of Damage Mechanics, 2010, 19(6): 727-751.
[16]
O’Higgins R M, Mccarthy C T,McCarthy M A. Identiflcation of damage and plasticity parameters for continuum damage mechanics modelling of carbon and glass fibre-reinforced composite materials [J]. Strain, 2011, 47(1): 105-115.
[17]
张 彦. 纤维增强复合材料层合结构冲击损伤预测研究[D]. 上海: 上海交通大学, 2007. Zhang Yan. Study on impact damage prediction in fiber reinforced composite laminated structures[D]. Shanghai:Shanghai Jiaotong University, 2007.
[18]
ASTM D3518/D3518 M-94 Standard test method for in-plane shear response of polymer matrix composite materials by tensile test of a ±45 laminate [S]. USA: ASTM, 2001.
[19]
ASTM Standard D3039/D3039 M-00 Standard test method for tensile proper ties of polymer rmatrix composite [S]. USA: ASTM, 2000.
[20]
Hill R. The mathematical theory of plasticity [M]. London: Oxford University Press, 1950.