Effect of nano-silica on fatigue behavior of glass fiber-reinforced epoxy composite laminates: A Weibull distribution approach

被引:12
作者
Gupta, Akash [1 ]
Singh, Manjeet [1 ,3 ]
Saini, J. S. [2 ]
机构
[1] Lovely Profess Univ, Sch Mech Engn, Phagwara, Punjab, India
[2] Thapar Inst Engn & Technol, Mech Engn Dept, Patiala, Punjab, India
[3] Lovely Profess Univ, Sch Mech Engn, Phagwara 144411, Punjab, India
关键词
cyclic loading; damage pattern; fatigue behavior; Fiber Reinforced Polymer (FRP) composite laminate; glass-reinforced epoxy composite; nano-particles; MECHANICAL-PROPERTIES; FAILURE ANALYSIS; PREDICTION; STRENGTH; LIFE;
D O I
10.1002/pc.27761
中图分类号
TB33 [复合材料];
学科分类号
摘要
The aim of this study is to assess the impact of nano-silica in glass fiber-reinforced epoxy composite (GFEC) subjected to static and fatigue loading. Laminates were prepared in compression molding machine followed by the tensile test and tension-tension fatigue testing at five different stress levels (from 50% to 90% of ultimate tensile strength). The addition of 3 wt% of nano-silica with epoxy improved the tensile and fatigue strength as compared to neat GFEC. Scanning electron microscope (SEM) images of the fractured specimen showed the damage pattern which indicates that neat GFEC laminate exhibited damage patterns characterized by fiber breakage and matrix cracking. On the other hand, the modified GFEC with nano-silica showed damage patterns including fiber pullout accompanied by fiber breakage and matrix cracking. During cyclic loading, the stress-strain hysteresis loop shows a reduced slope, indicating a decrease in the dynamic modulus of the specimen. This reduction in slope signifies a loss of stiffness during cyclic loading, particularly at high-stress levels. The highest dynamic modulus at high-stress levels indicates a rapid progression of severe damage and a shorter fatigue life. On the other hand, at low-stress levels, the lower magnitude of dynamic modulus suggests a moderate damage progression and a longer fatigue life.
引用
收藏
页码:9129 / 9140
页数:12
相关论文
共 43 条
[1]  
Ahmad Z, 1997, J APPL POLYM SCI, V63, P1345, DOI 10.1002/(SICI)1097-4628(19970307)63:10<1345::AID-APP14>3.3.CO
[2]  
2-Z
[3]   Failure analysis of two-dimensional carbon-epoxy composite plate pinned joint [J].
Aktas, A ;
Karakuzu, R .
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES, 1999, 6 (04) :347-361
[4]   The fatigue of carbon fibre reinforced plastics - A review [J].
Alam, Parvez ;
Mamalis, Dimitrios ;
Robert, Colin ;
Floreani, Christophe ;
Bradaigh, Conchur M. O. .
COMPOSITES PART B-ENGINEERING, 2019, 166 :555-579
[5]  
Arguelles A., 2022, SCI REP-UK, V12, P1, DOI [10.1038/s41598-022-23378-4, DOI 10.1038/S41598]
[6]   Behavior of pin-loaded laminated composites [J].
Baba, B. Okutan .
EXPERIMENTAL MECHANICS, 2006, 46 (05) :589-600
[7]   Statistical analysis of the mechanical properties of composite materials [J].
Barbero, E ;
Fernández-Sáez, J ;
Navarro, C .
COMPOSITES PART B-ENGINEERING, 2000, 31 (05) :375-381
[8]   Thermomechanical behavior of PA6.6 composites subjected to low cycle fatigue [J].
Benaarbia, Adil ;
Chrysochoos, Andre ;
Robert, Gilles .
COMPOSITES PART B-ENGINEERING, 2015, 76 :52-64
[9]   Fatigue life prediction of carbon fibre reinforced laminates by using cycle-dependent classical laminate theory [J].
Brunbauer, Julia ;
Pinter, Gerald .
COMPOSITES PART B-ENGINEERING, 2015, 70 :167-174
[10]   S-N Curve Models for Composite Materials Characterisation: An Evaluative Review [J].
Burhan, Ibrahim ;
Kim, Ho Sung .
JOURNAL OF COMPOSITES SCIENCE, 2018, 2 (03)