Quasi-static mode II fracture tests and simulations of Z-pinned woven composites

被引:30
作者
Huang, H. Sam [1 ]
Waas, Anthony M. [2 ,3 ,4 ]
机构
[1] SUNY Stony Brook, Dept Mech Engn, Stony Brook, NY USA
[2] Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA
[3] Univ Michigan, Dept Mech Engn, Ann Arbor, MI 48109 USA
[4] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7, England
关键词
Fracture; Woven composites; Mode II; Cohesive models; Z-pins; ADHESIVELY-BONDED STRUCTURES; PART; TOUGHNESS; PINS;
D O I
10.1016/j.engfracmech.2014.05.002
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Experimental results from quasi-static mode II ENF (end notch flexure) fracture tests for Z-pinned woven composites are used to investigate the influence of Z-pin density and Z-pin diameter on Mode II fracture toughness. The experimental results show that the 2% Z-pin composite and the 3% Z-pin composite have larger fracture toughness than the 1% Z-pin composite and a composite without Z-pins. Crack propagation changes from unstable propagation to stable propagation (crack arrest) as the Z-pin density increases. The additional fracture toughness provided by Z-pins prevents the primary crack to further propagate, enabling secondary and tertiary cracks to consume additional energy. While the primary crack is held from propagating by the frictional forces provided by Z-pins, the matrix in the composite is driven into the plastic state and enables the composite to absorb more energy. For numerical simulations, a discrete cohesive zone model (DCZM) is used to perform simulations. The simulations in conjunction with experimental results provide critical fracture toughness values. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:155 / 165
页数:11
相关论文
共 27 条
[1]   The estimate of the effect of z-pins on the strain release rate, fracture and fatigue in a composite co-cured z-pinned double cantilever beam [J].
Byrd, LW ;
Birman, V .
COMPOSITE STRUCTURES, 2005, 68 (01) :53-63
[2]  
Chang P, 2008, COMPOS PART A-APPL S, V38, P244
[3]  
Chou T.-W., 1992, MICROSTRUCTURAL DESI
[4]   Constitutive model for a fiber tow bridging a delamination crack [J].
Cox, BN .
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES, 1999, 6 (02) :117-138
[5]   Experimental study on z-pin bridging law by pullout test [J].
Dai, SC ;
Yan, WY ;
Liu, HY ;
Mai, YW .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (16) :2451-2457
[6]  
FREITAS G, 1994, J ADV MATER, V25, P36
[7]  
Freitas G, 1996, P 83 M AGARD SMP BOL
[8]  
Freitas G., 1991, P 9 DOD NASA FAA C C, P2657
[9]   Prediction of stiffness and stresses in z-fibre reinforced composite laminates [J].
Grassi, M ;
Zhang, X ;
Meo, M .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2002, 33 (12) :1653-1664
[10]   Evaluation of toughening concepts at structual features in CFRP - Part 1: Stiffener pull-off [J].
Greenhalgh, Emile ;
Lewis, Aaron ;
Bowen, Richard ;
Grassi, Marcello .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2006, 37 (10) :1521-1535