Effect of impact damage on the curved beam interlaminar strength of carbon/epoxy laminates

被引:26
作者
Hao, Wenfeng [1 ]
Yuan, Yanan [2 ]
Zhu, Jianguo [1 ]
Chen, Lei [1 ]
机构
[1] Jiangsu Univ, Fac Civil Engn & Mech, Zhenjiang, Jiangsu, Peoples R China
[2] Tsinghua Univ, Dept Engn Mech, Appl Mech Lab, Beijing 100084, Peoples R China
基金
中国国家自然科学基金;
关键词
low velocity impact; digital speckle correlation method; Composite laminates; four-point bending; interlaminar strength; LOW FIBER-VOLUME; FLEXURAL PROPERTIES; COMPOSITE PLATES; DEFORMATION; PREDICTION; RESISTANCE;
D O I
10.1080/01694243.2016.1144261
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
The bending interlaminar strength and bending interlaminar strength after impact of carbon/epoxy-laminated curved beams were studied experimentally using four-point bending test and low velocity impact. First, the post- impact damage of the laminated curved beams with different radii was analyzed based on ultrasonic C-scan images. Then, the effect of impact damage on both the interlaminar strength and the maximum interlaminar radial stresses of the laminated curved beams were investigated. Finally, the full-field displacement distributions of the laminated curved beams were obtained using digital speckle correlation method. Four-point bending experimental results play a significant role for interlaminar strength in evaluating the laminated curved beams with and without impact damage.
引用
收藏
页码:1189 / 1200
页数:12
相关论文
共 29 条
[1]  
[Anonymous], D6415D6415M ASTM INT
[2]   The response of laminated composite plates under low-velocity impact loading [J].
Aslan, Z ;
Karakuzu, R ;
Okutan, B .
COMPOSITE STRUCTURES, 2003, 59 (01) :119-127
[3]   Shear Lag in Fiber-Reinforced Plastics Composite Simply Supported II-Beams [J].
Chen, Hao-Sen ;
Zhao, Qi-Lin ;
Gu, Yu ;
Yin, Ya-Jun ;
Fang, Dai-Ning .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2013, 20 (07) :564-570
[4]   Impact dynamics and damage in composite structures [J].
Christoforou, AP .
COMPOSITE STRUCTURES, 2001, 52 (02) :181-188
[5]   Failure mechanisms on composite specimens subjected to compression after impact [J].
de Freitas, M ;
Reis, L .
COMPOSITE STRUCTURES, 1998, 42 (04) :365-373
[6]   An experimental investigation on the impact response of composite materials [J].
Evci, Celal ;
Gulgec, Mufit .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2012, 43 :40-51
[7]   Experimental investigation on deformation and strength of carbon/epoxy laminated curved beams [J].
Hao, Wenfeng ;
Ge, Dongyun ;
Ma, Yinji ;
Yao, Xuefeng ;
Shi, Yue .
POLYMER TESTING, 2012, 31 (04) :520-526
[8]   Effect of impact damage on the compressive response of composite laminates [J].
Hawyes, VJ ;
Curtis, PT ;
Soutis, C .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2001, 32 (09) :1263-1270
[9]  
Huang Y, 2008, J REINF PLAST COMP, V2, P165
[10]   Effects of mechanical and geometrical properties of adhesive and metal layers on low-velocity impact behavior of metal laminate structures [J].
Khoramishad, Hadi ;
Tofighi, Mohammad Bagheri .
JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2015, 29 (07) :592-608