Influence of temperature on the delamination process under mode I fracture and dynamic loading of two carbon-epoxy composites

被引:24
作者
Argueelles, A. [1 ]
Vina, J. [2 ]
Canteli, A. F. [1 ]
Coronado, P. [1 ]
Mollon, V. [2 ]
机构
[1] Univ Oviedo, Dept Construct & Mfg Engn, Gijon 33203, Spain
[2] Univ Oviedo, Dept Mat Sci & Met Engn, Gijon 33203, Spain
关键词
Delamination; Fracture; Statistical properties/methods; FIBER-REINFORCED COMPOSITES; GENERAL REGRESSION-MODEL; FATIGUE; BEHAVIOR; POLYMER; GROWTH; TOUGHNESS;
D O I
10.1016/j.compositesb.2014.08.051
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper experimentally analyzes the influence of temperature and type of matrix on the delamination process of two composites subjected to fatigue loading through the study of their fracture under mode I behavior. The materials were manufactured with the same AS4 unidirectional carbon reinforcement and two epoxy matrices with different fracture behavior. The chosen temperatures for the experiments were 20 (room temperature), 50 and 90 degrees C. The experimental study carried out under dynamic loading enabled the authors to determine the influence that temperature has on the onset of delamination for the entire range of fatigue life of the material, from the low number of cycles zone to the high number of cycles zone. That is, it enabled the plotting of fatigue curves, represented as G(lmax)-N (number of cycles required for the onset of delamination given a certain energy release rate) for an asymmetry coefficient of 0.2 (the ratio between the maximum and minimum fracture energies applied during the dynamic tests). The experimental data obtained were treated with a probabilistic model based on a Weibull distribution which allowed the identification of relevant aspects of the fatigue behavior of the materials such as the estimation of fatigue strength for periods greater than the tested values and the analysis of the reliability of the results. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:207 / 214
页数:8
相关论文
共 34 条
[1]  
American Society For Testing And Materials, 2008, ASTM D3039: Test Method for Tensile Properties of Polymer Matrix Composite Materials, DOI [10.1520/D3039_D3039M-08, DOI 10.1520/D3039_D3039M-08]
[2]  
[Anonymous], 2011, D611597 ASTM, DOI DOI 10.1520/D6115-97R11
[3]  
[Anonymous], 2013, D552813 ASTM, DOI [10.1520/D5528-01R07E03, DOI 10.1520/D5528-01R07E03]
[4]  
[Anonymous], PROF COD
[5]  
[Anonymous], 2013, D351813 ASTM INT, DOI DOI 10.1520/D3518_D3518M
[6]   Evolution of the impact strength of carbon fiber-reinforced PEI following exposure to mechanical, hygrothermal and hygrothermomechanical aging [J].
Argueelles, A. ;
Fernandez-Canteli, A. ;
Vina, J. ;
Garcia, M. A. .
JOURNAL OF COMPOSITE MATERIALS, 2007, 41 (19) :2337-2346
[7]   Using a statistical model for the analysis of the influence of the type of matrix carbon-epoxy composites on the fatigue delamination under modes I and II of fracture [J].
Argueelles, A. ;
Coronado, P. ;
Canteli, A. F. ;
Vina, J. ;
Bonhomme, J. .
INTERNATIONAL JOURNAL OF FATIGUE, 2013, 56 :54-59
[8]   Influence of Resin Type on the Delamination Behavior of Carbon Fiber Reinforced Composites Under Mode-II Loading [J].
Argueelles, A. ;
Vina, J. ;
Canteli, A. F. ;
Bonhomme, J. .
INTERNATIONAL JOURNAL OF DAMAGE MECHANICS, 2011, 20 (07) :963-978
[9]   Influence of the matrix constituent on mode I and mode II delamination toughness in fiber-reinforced polymer composites under cyclic fatigue [J].
Argueelles, A. ;
Vina, J. ;
Fernandez-Canteli, A. ;
Vina, I. ;
Bonhomme, J. .
MECHANICS OF MATERIALS, 2011, 43 (01) :62-67
[10]   Mode I fracture of epoxy bonded composite joints: 1. Quasi-static loading [J].
Ashcroft, IA ;
Hughes, DJ ;
Shaw, SJ .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2001, 21 (02) :87-99