基于弹塑性损伤本构模型的复合材料层合板破坏荷载预测
Failure loads prediction of composite laminates using a combined elastoplastic damage model

DOI: 10.13801/j.cnki.fhclxb.20160721.001

Keywords: 复合材料本构模型,渐进失效分析,塑性效应,刚度退化,隐式积分算法
composite material constitutive model,progressive failure analysis,plasticity effects,stiffness degradation,implicit integration algorithm

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[1]	LAFARIE-FRENOT M C, TOUCHARD F. Comparative in-plane shear behaviour of long-carbon-fibre composites with thermoset and thermoplastic matrix[J]. Composites Science and Technology, 1994, 52(3):417-425.
[2]	MATZENMILLER A, LUBLINER J, TAYLOR R L. A constitutive model for anisotropic damage in fiber-composites[J]. Mechanics of Materials, 1995, 20(2):125-152.
[3]	LAPCZYK I, HURTADO J A. Progressive damage modeling in fiber-reinforced materials[J]. Composites Part A, 2007, 38(11):2333-2341.
[4]	MAIMí P, CAMANHO P P, MAYUGO J A, et al. A continuum damage model for composite laminates:Part I-Constitutive model[J]. Mechanics of Materials, 2007, 39(10):897-908.
[5]	MAIMí P, CAMANHO P P, MAYUGO J A, et al. A continuum damage model for composite laminates:Part II-Computational implementation and validation[J]. Mechanics of Materials, 2007, 39(10):909-919.
[6]	庄茁, 宋恒旭, 彭涛等. 复合材料低速冲击损伤研究及等效模型的应用[J]. 工程力学, 2012, 29(增刊II):15-22. ZHUANG Z, SONG H X, PENG T, et al. Damage of composite under low-velocity impact and application of mechanical equivalent model[J]. Engineering Mechanics, 2012, 29(SII):15-22(in Chinese).
[7]	吴义韬, 姚卫星, 吴富强. 复合材料层合板面内渐进损伤分析的CDM模型[J]. 力学学报, 2014, 46(1):94-104. WU Y T, YAO W X, WU F Q. CDM model for intralaminar progressive damage analysis of composite laminates[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(1):94-104(in Chinese).
[8]	LADEVEZE P, LE DANTEC E. Damage modelling of the elementary ply for laminated composites[J]. Composites Science and Technology, 1992, 43(3):257-267.
[9]	MAA R H, CHENG J H. A CDM-based failure model for predicting strength of notched composite laminates[J]. Com-posites Part B, 2002, 33(6):479-489.
[10]	American Society for Testing and Materials. D5528-01 Standard test methods for mode I interlaminar fracture toughness of unidirectional fibre-reinforced polymer matrix composites[S]. West Conshohocken:Annu. Book ASTM Stand, 2007.
[11]	CAMANHO P P, MAIMí P, DAVILA C G. Prediction of size effects in notched laminates using continuum damage mechanics[J]. Composites Science and Technology, 2007, 67(13):2715-2727.
[12]	CHEN J F, MOROZOV E V, SHANKAR K. Simulating progressive failure of composite laminates including in-ply and delamination damage effects[J]. Composites:Part A, 2014, 61:185-200.
[13]	PHAM D C, SUN X S, TAN V B V, et al. Progressive failure analysis of scaled double-notched carbon/epoxy com-posite laminates[J]. International Journal of Damage Mecha-nics, 2012, 21(8):1154-1185.
[14]	WU P S, SUN C T. Bearing failure in pin contact of com-posite laminates[J]. AIAA Journal, 1998, 36(11):2124-2129.
[15]	PAEPEGEM W V, DE BAERE I, DEGRIECK J. Modelling the nonlinear shear stress-strain response of glass fibre-reinforced composites. Part I:Experimental results[J]. Composites Science and Technology, 2006, 66(10):1455-1464.
[16]	RIBEIRO M L, TITA V, VANDEPITTE D. A new damage model for composite laminates[J]. Composite Structures, 2012, 94(2):635-642.
[17]	WILLIAMS KV, VAZIRI R. Application of a damage mechanics model for predicting the impact response of composite materials[J]. Computers & Structures, 2001, 79(10):997-1011.
[18]	XIAO X. Modeling energy absorption with a damage mechanics based composite material model[J]. Journal of Composite Materials, 2009, 43(5):427-444.
[19]	CHEN J F, MOROZOV E V, SHANKAR K. A combined elastoplastic damage model for progressive failure analysis of composite materials and structures[J]. Composite Struc-tures, 2012, 94(12):3478-3489.
[20]	SUN C T, CHEN J L. A simple flow rule for characterizing nonlinear behavior of fiber composites[J]. Journal of Composite Materials, 1989, 23(10):1009-1020.
[21]	HASHIN Z. Failure criteria for unidirectional fiber compo-sites[J]. Journal of Applied Mechanics-T ASME, 1980, 47(2):329-334.
[22]	FARIA R, OLIVER J, CERVERA M. A strain-based plastic viscous-damage model for massive concrete structures[J]. International Journal of Solids and Structures, 1998, 35(14):1533-1558.
[23]	LAFFAN M J, PINHO S T, ROBINSON P, et al. Translaminar fracture toughness testing of composites:A review[J]. Polymer testing. 2012, 31(3):481-489.
[24]	Dassault Systèmes. 32.5.6 Defining the constitutive response of cohesive elements using a traction-separation description[CP]. Abaqus Analysis User's Guide, Simulia Abaqus 6.14 docu-mentation.
[25]	CAMANHO P P, DAVILA C G. Analysis of the effects of residual strains and defects on skin/stiffener debonding using decohesion elements[C]. SDM Conference. Norfolk, VA, 2003.
[26]	Dassault Systèmes. 24.3 Damage and failure for fiber-reinforced composites[CP]. Abaqus Analysis User's Guide, Simulia Abaqus 6.14 documentation.
[27]	LINDE P, PLEITNER J, DE BOER H, et al. Modelling and simulation of fiber metal laminates[C]. ABAQUS Users' Conference, 2004.
[28]	Dassault Systèmes. 1.4.6 Failure of blunt notched fiber metal laminates[CP]. Abaqus Example Problems Guide, Simulia Abaqus 6.14 documentation.
[29]	VAN DER MEER F P, OLIVER C, SLUYS L J. Computational analysis of progressive failure in a notched laminate including shear nonlinearity and fiber failure[J]. Composites Science and Technology, 2010, 70(4):692-700.
[30]	FLATSCHER T, PETTERMANN H E. A constitutive model for fiber-reinforced polymer plies accounting for plasti-city and brittle damage including softening-Implementation for implicit FEM[J]. Composite Structures, 2011, 93(9):2241-2249.
[31]	BAZANT Z, OH B. Crack band theory for fracture of concrete[J]. Materials and Structures, 1983, 16(3):155-177.
[32]	PINHO S T, ROBINSON P, IANNUCCI L. Fracture toughness of the tensile and compressive fibre failure modes in laminated composites[J]. Composites Science and Tech-nology, 2006, 66(13):2069-2079.
[33]	PINHO S T, ROBINSON P, IANNUCCI L. Developing a four point bend specimen to measure the mode I intralaminar fracture toughness of unidirectional laminated composites[J]. Composites Science and Technology, 2009, 69(7-8):1303-1309.
[34]	CZABAJ M W, RATCLIFFE J G. Comparison of intra-laminar and interlaminar Mode-I fracture toughness of unidi-rectional IM7/8552 graphite/epoxy composite[R]. Technical Report NF1676L-15094. NASA Langley Research Center, Hampton, VA, United States, 2012.

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