Low-velocity impact behavior of glass fiber epoxy composites modified with nanoceramic particles

被引:14
作者
Kallagunta, Harish [1 ,2 ]
Tate, Jitendra S. [1 ,2 ]
机构
[1] Texas State Univ, Mat Sci Engn & Commercializat, San Marcos, TX USA
[2] Texas State Univ, Ingram Sch Engn, San Marcos, TX USA
关键词
Low-velocity impact; dynamic failure; elass epoxy composites; alumina nanofibers; nanosilica; thermography; TENSILE PROPERTIES; NANOPARTICLES; SILICA;
D O I
10.1177/0021998319893435
中图分类号
TB33 [复合材料];
学科分类号
摘要
The introduction of new type of nanomaterials has provided challenges in a deeper level understanding of mechanical behavior and failure mechanisms of fiber-reinforced composites. In this study, a comparison of low-velocity impact behavior of E-Glass epoxy composites modified with 10 wt% nanosilica and 2.5 wt% Nafen (TM) alumina nanofibers manufactured using vacuum-assisted resin transfer molding is reported. Low-velocity impact tests at three impact energies of 29 J, 39 J, and 50 J are conducted and impact responses, such as impact strength, absorbed energy, and damage area are determined and compared for the two nanoparticles. The damage sustained by composite samples is evaluated by optical microscopy and infrared thermography. Nanosilica-incorporated composites showed rigid behavior, whereas alumina nanofiber-modified composites showed increased stiffness at increased energy of impact as observed from the initial stiffness and deflection of samples. The degree of damage in case of 10 wt% nanosilica-modified composites is reduced by 7.04%, 3.96%, and 7.92% for energy levels of 29 J, 39 J, and 50 J respectively when compared to nonmodified composites, whereas 2.5 wt% alumina nanofiber-modified composites showed 1.66%, -7.35%, and 26.39% for energy levels of 29 J, 39 J, and 50 J, respectively.
引用
收藏
页码:2217 / 2228
页数:12
相关论文
共 19 条
[1]   Influence of the laminate thickness in low velocity impact behavior of composite material plate [J].
Belingardi, G ;
Vadori, R .
COMPOSITE STRUCTURES, 2003, 61 (1-2) :27-38
[2]  
Bolick RL, 2007, P SAMPE EUR 28 INT C
[3]   Toughening of epoxy-based hybrid nanocomposites [J].
Carolan, D. ;
Ivankovic, A. ;
Kinloch, A. J. ;
Sprenger, S. ;
Taylor, A. C. .
POLYMER, 2016, 97 :179-190
[4]   Predicting delamination and debonding in modern aerospace composite structures [J].
Davies, GAO ;
Hitchings, D ;
Ankersen, J .
COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (06) :846-854
[5]   The effects of nano-silica/nano-alumina on fatigue behavior of glass fiber-reinforced epoxy composites [J].
Fathy, A. ;
Shaker, A. ;
Hamid, M. Abdel ;
Megahed, A. A. .
JOURNAL OF COMPOSITE MATERIALS, 2017, 51 (12) :1667-1679
[6]  
Hao Wu JHK, 2015, SOC ADV MAT PROC ENG
[7]   Tensile properties of nanosilica/epoxy nanocomposites [J].
Jumahat, Aidah ;
Soutis, Costas ;
Abdullah, Shahrul Azam ;
Kasolang, Salmiah .
INTERNATIONAL SYMPOSIUM ON ROBOTICS AND INTELLIGENT SENSORS 2012 (IRIS 2012), 2012, 41 :1634-1640
[8]   Fatigue crack propagation behaviour of epoxy resins modified with silica-nanoparticles [J].
Kothmann, M. H. ;
Zeiler, R. ;
de Anda, A. Rios ;
Brueckner, A. ;
Altstaedt, V. .
POLYMER, 2015, 60 :157-163
[9]   Single carbon fiber fracture embedded in an epoxy matrix modified by nanoparticles [J].
Liu, Luqi ;
Li, Lingyun ;
Gao, Yun ;
Tang, Longcheng ;
Zhang, Zhong .
COMPOSITES SCIENCE AND TECHNOLOGY, 2013, 77 :101-109
[10]   Infrared thermography to evaluate impact damage in glass/epoxy with manufacturing defects [J].
Meola, Carosena ;
Carlomagno, Giovanni M. .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2014, 67 :1-11