Hybridization effects on quasi-static penetration resistance in fiber reinforced hybrid composite laminates

被引:69
作者
Bulut, Mehmet [1 ]
Erklig, Ahmet [1 ]
Yeter, Eyup [2 ]
机构
[1] Gaziantep Univ, Dept Mech Engn, Fac Engn, TR-27310 Gaziantep, Turkey
[2] Gaziantep Univ, Fac Aeronaut & Aerosp, Aircraft & Aerosp Engn Dept, TR-27310 Gaziantep, Turkey
关键词
Hybrid; Composite; Fiber; Penetration; LOW-VELOCITY IMPACT; BALLISTIC IMPACT; FLEXURAL PROPERTIES; S-2; GLASS; DAMAGE; BEHAVIOR; INDENTATION; PREDICTION; DELAMINATION; PERFORATION;
D O I
10.1016/j.compositesb.2016.05.025
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Quasi static penetration tests (QSPT) were conducted on fiber reinforced hybrid composite laminates with a circular and cylindrical punch. Woven Carbon, Kevlar and S-glass fibers were used as reinforcing fibers for production of hybrid and non-hybrid composite laminates. Punch shear test procedures were employed until the perforation and complete plugging shear out of the laminate. During QSPT experiments, a flat end punch with diameter of 12.7 mm has been used for two different support spans (25.4 and 63.5 mm) to obtain two different support span (D-s) to punch diameter (D-p) ratios (SPR = D-s/D-p = 2 and 5). After the experiments, the extent of compression-shear and tension-shear based failure modes were characterized at constant punch displacements of 8 and 10 mm for SPR = 2 and 5, respectively. In addition to visualize of front and back side surfaces, composite samples were half sectioned at damage region to observe the amount of delamination and damage through the thickness of the laminate. It was found that hybridization effects were distinctly observed with dominated tension-shear damage mode at SPR = 5. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:9 / 22
页数:14
相关论文
共 43 条
[1]   The Effect of Hybridization on the GFRP Behavior under Quasi-Static Penetration [J].
Al-Kinani, R. ;
Najim, F. ;
de Moura, M. F. S. F. .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2014, 21 (02) :81-87
[2]  
[Anonymous], 2012, D6264D6264M12 ASTM
[3]  
[Anonymous], 2002, D73202 ASTM
[4]   The effect of hybridization on the ballistic impact behavior of hybrid composite armors [J].
Bandaru, Aswani Kumar ;
Vetiyatil, Lakshmi ;
Ahmad, Suhail .
COMPOSITES PART B-ENGINEERING, 2015, 76 :300-319
[5]   Low velocity impact tests of laminate glass-fiber-epoxy matrix composite material plates [J].
Belingardi, G ;
Vadori, R .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2002, 27 (02) :213-229
[6]  
Critescu N., 1975, FOREIGN OBJECT IMPAC, P159
[7]   Prediction of threshold impact energy for onset of delamination in quasi-isotropic carbon/epoxy composite laminates under low-velocity impact [J].
Davies, GAO ;
Hitchings, D ;
Wang, J .
COMPOSITES SCIENCE AND TECHNOLOGY, 2000, 60 (01) :1-7
[8]  
Deka LJ, 2008, THESIS
[9]   Energy-based approach to impact damage in CFRP laminates [J].
Delfosse, D ;
Poursartip, A .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1997, 28 (07) :647-655
[10]   Flexural and tensile strengths of unidirectional hybrid epoxy composites reinforced by S-2 glass and T700S carbon fibres [J].
Dong, Chensong ;
Davies, Ian J. .
MATERIALS & DESIGN, 2014, 54 :955-966