Micromechanical damage modeling and multiscale progressive failure analysis of composite pressure vessel

被引:44
作者
Liu, P. F. [1 ]
Chu, J. K. [1 ]
Hou, S. J. [1 ]
Zheng, J. Y. [1 ]
机构
[1] Zhejiang Univ, Inst Chem Machinery & Proc Equipment, Hangzhou 310027, Zhejiang, Peoples R China
关键词
Micromechanical damage model; Multiscale failure analysis; Finite element analysis; Composite laminates; FIBER-REINFORCED COMPOSITES; MECHANICAL-BEHAVIOR; ANISOTROPIC DAMAGE; CONSTITUTIVE MODEL; EPOXY COMPOSITE; LOAD-TRANSFER; PART I; PREDICTION; EVOLUTION; STRENGTH;
D O I
10.1016/j.commatsci.2012.03.015
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A multiscale damage model is proposed to predict the failure properties and ultimate burst pressure of composite pressure vessel. The macroscopic damage evolution and stiffness properties of the composite vessel are represented by those of the representative volume element (RVE). First, a microscopic damage model is established, where the fiber breakage is predicted using Monte Carlo simulation, and the progressive matrix cracking is described by continuum damage mechanics-based modeling and the interface failure is simulated using Xu and Needleman's cohesive model. Then, a stiffness degradation model is proposed to link the macroscopic stiffness of the composite vessel with the failure evolvement of the RVE. Finally, the multiscale progressive failure analysis of the composite vessel is implemented by associating the finite element codes ANSYS-APDL with ABAQUS-UMAT. The numerical convergence problems are effectively addressed by introducing the viscous damping effect. The predicted failure strengths of the composite vessels are consistent with the experimental results. (C) 2012 Elsevier B.V. All rights reserved.
引用
收藏
页码:137 / 148
页数:12
相关论文
共 50 条
[1]  
[Anonymous], CONTINUUM MECH
[2]  
[Anonymous], 2005, Engineering Damage Mechanics
[3]   A constitutive model for elastic damage in fiber-reinforced PMC laminae [J].
Barbero, EJ ;
De Vivo, L .
INTERNATIONAL JOURNAL OF DAMAGE MECHANICS, 2001, 10 (01) :73-93
[4]  
Barenblatt GI, 1962, Adv Appl Mech, V7, P55, DOI [10.1016/S0065-2156(08)70121-2, DOI 10.1016/S0065-2156(08)70121-2]
[5]   Prediction of progressive failure in multidirectional composite laminated panels [J].
Basu, Shiladitya ;
Waas, Anthony M. ;
Ambur, Damodar R. .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2007, 44 (09) :2648-2676
[6]   Micromechanisms of load transfer in a unidirectional carbon fibre-reinforced epoxy composite due to fibre failures. Part 1: Micromechanisms and 3D analysis of load transfer: The elastic case [J].
Blassiau, S ;
Thionnet, A ;
Bunsell, AR .
COMPOSITE STRUCTURES, 2006, 74 (03) :303-318
[7]   Micromechanisms of load transfer in a unidirectional carbon fibre-reinforced epoxy composite due to fibre failures: Part 3. Multiscale reconstruction of composite behaviour [J].
Blasslau, S. ;
Thionnet, A. ;
Bunsell, A. R. .
COMPOSITE STRUCTURES, 2008, 83 (03) :312-323
[8]   PLASTIC-FLOW OF ISOTROPIC POLYMERS [J].
BOWDEN, PB ;
JUKES, JA .
JOURNAL OF MATERIALS SCIENCE, 1972, 7 (01) :52-&
[9]   An anisotropic ductile damage model based on irreversible thermodynamics [J].
Brünig, M .
INTERNATIONAL JOURNAL OF PLASTICITY, 2003, 19 (10) :1679-1713
[10]   Life prediction for carbon fibre filament wound composite structures [J].
Bunsell, A. R. ;
Thionnet, A. .
PHILOSOPHICAL MAGAZINE, 2010, 90 (31-32) :4129-4146