Interfacial fracture of the fibre-metal laminates based on fibre reinforced thermoplastics

被引:52
作者
Abdullah, M. R. [1 ]
Prawoto, Y. [2 ]
Cantwell, W. J. [3 ,4 ]
机构
[1] UTM, Fac Mech Engn, Skudai 81310, Johor, Malaysia
[2] Surya Univ, Dept Phys Energy Engn, Summarecon Serpong Tange 15810, Indonesia
[3] KUSTAR, Dept Aerosp Engn, Abu Dhabi, U Arab Emirates
[4] Univ Liverpool, Dept Engn, Liverpool L69 3BX, Merseyside, England
关键词
Fibre-metal laminates; Interfacial fracture energy; Fibre bridging; Stress intensity factor; AIRCRAFT STRUCTURES; POLYPROPYLENE; COMPOSITE; BEHAVIOR; GLARE;
D O I
10.1016/j.matdes.2014.03.058
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
As the adhesion quality plays an important role in determining the mechanical performance and environmental stability of most types of fibre-metal laminates (FMLs), investigating the interfacial fracture properties becomes one of the key factors for the improvement. Adhesion of a self-reinforced polypropylene (SRPP) and glass fibre reinforced polypropylene (GFPP) based FML is evaluated experimentally. Single Cantilever Beam (SCB) tests were performed to access interfacial fracture energy (G(c)) of the bi-material laminates and their associated interlayer materials. Simulations mimicking the experiments were also performed. The energy needed to fracture was obtained experimentally and also via stress intensity factor from the simulations. The test results show that good adhesion between the aluminium and fibre reinforced thermoplastics can be achieved using a sulphuric acid anodising surface pre-treatment. Further examination has shown that the edges of the test samples highlighted the presence of significant fibre bridging in the SRPP and plastics deformation in the GFPP. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:446 / 452
页数:7
相关论文
共 21 条
[1]   The impact resistance of fiber-metal laminates based on glass fiber reinforced polypropylene [J].
Abdullah, M. R. ;
Cantwell, W. J. .
POLYMER COMPOSITES, 2006, 27 (06) :700-708
[2]   Fatigue and damage tolerance issues of Glare in aircraft structures [J].
Alderliesten, R. C. ;
Homan, J. J. .
INTERNATIONAL JOURNAL OF FATIGUE, 2006, 28 (10) :1116-1123
[3]  
Cantwell WJ, 2002, HI PER STRUCT MAT, V4, P33
[4]  
Cantwell WJ, 2005, ICCST 5 SHARJ
[5]  
Cantwell WJ, 2001, HIGH VELOCITY IMPACT, V250, P1
[6]  
Carillo jG, 2007, THESIS U LIVERPOOL
[7]   Mechanical properties of a novel fiber-metal laminate based on a polypropylene composite [J].
Carrillo, J. G. ;
Cantwell, W. J. .
MECHANICS OF MATERIALS, 2009, 41 (07) :828-838
[8]   The impact properties of high-temperature fiber-metal laminates [J].
Cortes, P. ;
Cantwell, W. J. .
JOURNAL OF COMPOSITE MATERIALS, 2007, 41 (05) :613-632
[10]  
Davies P, 1991, STP 1110 COMPOSITE M, V3, P70, DOI [10.1520/STP17713S, DOI 10.1520/STP17713S]