A micromechanics-based degradation model for composite progressive damage analysis

被引:48
作者
Zhang, Jianyu [1 ]
Zhou, Longwei [2 ]
Chen, Yuli [3 ]
Zhao, Libin [2 ]
Fei, Binjun [3 ]
机构
[1] Chongqing Univ, Coll Aerosp Engn, Chongqing 630044, Peoples R China
[2] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[3] Beihang Univ, Inst Solid Mech, Beijing 100191, Peoples R China
基金
国家高技术研究发展计划(863计划); 美国国家科学基金会;
关键词
Carbon fibers; structural composites; mechanical properties; damage mechanics; finite element analysis; MECHANICALLY FASTENED JOINTS; INDUCED LAMINATE FAILURE; BOLT-CLAMPING LOADS; OPEN-HOLE; STRENGTH PREDICTION; ELEMENT-FAILURE; FIBER WAVINESS; PART II; COMPRESSIVE FAILURE; TENSILE;
D O I
10.1177/0021998315602947
中图分类号
TB33 [复合材料];
学科分类号
摘要
A new material degradation model only with fundamental material properties required is proposed for composite progressive damage analysis based on micromechanics. For different failure modes, the effects of fiber and/or matrix damage on the composite material properties are explored, from which the material degradation factors for these failure modes are deduced. The material degradation model is then implemented for progressive damage analyses, using user subroutines in the commercial code ABAQUS (R), accompanying with a modified Hashin type failure criterion and finite element models for six commonly used double-lap composite bolted joints with various layups, geometry dimensions, and fasteners. The numerical predictions of failure loads, failure patterns, and load-displacement curves are compared with results obtained from static tests and further ultrasonic C-scan detection. Good agreements between numerical failure predictions and experimental outcomes indicate the effectiveness and suitability of the proposed model for progressive damage analyses of composite bolted joints.
引用
收藏
页码:2271 / 2287
页数:17
相关论文
共 64 条
[1]  
[Anonymous], 2013, D5961D5961M13 ASTM
[2]  
[Anonymous], 1967, POLYM MECH, DOI DOI 10.1007/BF00858855
[3]  
[Anonymous], 2003, MECH COMPOSITE STRUC, DOI DOI 10.1017/CBO9780511547140
[4]   Compressive failure of 0° unidirectional carbon-fibre-reinforced plastic (CFRP) laminates by fibre microbuckling [J].
Berbinau, P ;
Soutis, C ;
Guz, IA .
COMPOSITES SCIENCE AND TECHNOLOGY, 1999, 59 (09) :1451-1455
[5]   COMPRESSIVE FAILURE OF FIBER COMPOSITES [J].
BUDIANSKY, B ;
FLECK, NA .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 1993, 41 (01) :183-211
[6]   On kink-band propagation in fiber composites [J].
Budiansky, B ;
Fleck, NA ;
Amazigo, JC .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 1998, 46 (09) :1637-1653
[7]   A design methodology for mechanically fastened joints in laminated composite materials [J].
Camanho, P. P. ;
Lambert, M. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (15) :3004-3020
[8]   Modeling the inelastic deformation and fracture of polymer composites - Part II: Smeared crack model [J].
Camanho, P. P. ;
Bessa, M. A. ;
Catalanotti, G. ;
Vogler, M. ;
Rolfes, R. .
MECHANICS OF MATERIALS, 2013, 59 :36-49
[9]   A progressive damage model for mechanically fastened joints in composite laminates [J].
Camanho, PP ;
Matthews, FL .
JOURNAL OF COMPOSITE MATERIALS, 1999, 33 (24) :2248-2280
[10]  
Chan W.S., 1994, Journal of Thermoplastic Composite Materials, V7, P243, DOI 10.1177/089270579400700306