Effect of multiphase fiber system and stacking sequence on low-velocity impact and residual tensile behavior of glass/epoxy composite laminates

被引:36
作者
Jefferson, Andrew J. [1 ]
Srinivasan, Sivakumar M. [1 ]
Arockiarajan, A. [1 ]
机构
[1] Indian Inst Technol Madras, Dept Appl Mech, Madras, Tamil Nadu, India
关键词
HIGH-STRENGTH CONCRETE; DROP-WEIGHT IMPACT; HYBRID COMPOSITES; DAMAGE CHARACTERIZATION; MECHANICAL-PROPERTIES; RESISTANCE; BASALT; PLATES;
D O I
10.1002/pc.24884
中图分类号
TB33 [复合材料];
学科分类号
摘要
This article investigates the effect of multiphase fiber system based on plain weave woven fabrics and chopped short fibers in glass/epoxy composite laminates on low-velocity drop weight impact and quasi-static tensile after impact (TAI) behaviors. In this regard, glass/epoxy composites with two stacking sequences (intercalated and sandwich-like lay-ups) were tested and compared with homogeneous standard composites fabricated with either only woven or only chopped fibers. In all the samples with multiphase fiber system, the amount of woven and chopped glass fibers were equal (4 layers and 3 layers, respectively), while stacking sequences were different. This enabled us to investigate the associated influences of fiber architecture and stacking sequence on low-velocity drop weight impact and TAI behavior of the glass/epoxy composite laminates. All the glass/epoxy samples were impacted at four various impact energy levels, particularly 2, 4, 6, and 8 J. Results depicted that fiber architecture and stacking sequence played a vital role in low-velocity drop weight impact and TAI behavior (i.e., damage degree, absorbed energy, peak contact force, residual deformation, residual tensile strength, displacement to ultimate failure, and failure profile) of the glass/epoxy samples. The results depicted that the sandwich-like lay-up configuration presented superior impact properties and damage tolerance capabilities at low impact energies (up to 4 J). On the contrary, intercalated lay-up arrangement suited better to withstand widespread damage generated by higher impact energy levels (6 and 8 J), because they enabled a more efficient redistribution of low-velocity impact damage in the composite. POLYM. COMPOS., 40:1450-1462, 2019. (c) 2018 Society of Plastics Engineers
引用
收藏
页码:1450 / 1462
页数:13
相关论文
共 48 条
[1]  
Abrate S, 2011, CISM COURSES LECT
[2]   Impact damage on fibre-reinforced polymer matrix composite - A review [J].
Agrawal, Sandeep ;
Singh, Kalyan Kumar ;
Sarkar, P. K. .
JOURNAL OF COMPOSITE MATERIALS, 2014, 48 (03) :317-332
[3]   Modelling of impact forces and pressures in Lagrangian bird strike analyses [J].
Airoldi, A ;
Cacchione, B .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2006, 32 (10) :1651-1677
[4]   Response of hybrid-fiber reinforced concrete slabs to hard projectile impact [J].
Almusallam, Tarek H. ;
Siddiqui, Nadeem A. ;
Iqbal, Rizwan A. ;
Abbas, Husain .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2013, 58 :17-30
[5]   The role of adhesively bonded super hybrid external patches on the impact and post-impact response of repaired glass/epoxy composite laminates [J].
Andrew, J. Jefferson ;
Srinivasan, Sivakumar M. ;
Arockiarajan, A. .
COMPOSITE STRUCTURES, 2018, 184 :848-859
[6]   Quasi-static indentation properties of damaged glass/epoxy composite laminates repaired by the application of intra-ply hybrid patches [J].
Andrew, J. Jefferson ;
Arumugam, V. ;
Ramesh, C. ;
Poorani, S. ;
Santulli, C. .
POLYMER TESTING, 2017, 61 :132-145
[7]   Effect of patch hybridization on the tensile behavior of patch repaired glass/epoxy composite laminates using acoustic emission monitoring [J].
Andrew, J. Jefferson ;
Arumugam, V. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2017, 74 :155-166
[8]   Residual strength and damage characterization of repaired glass/epoxy composite laminates using AE and DIC [J].
Andrew, J. Jefferson ;
Arumugam, V. ;
Bull, D. J. ;
Dhakal, H. N. .
COMPOSITE STRUCTURES, 2016, 152 :124-139
[9]   Effect of post-cure temperature and different reinforcements in adhesive bonded repair for damaged glass/epoxy composites under multiple quasi-static indentation loading [J].
Andrew, J. Jefferson ;
Arumugam, V. ;
Santulli, C. .
COMPOSITE STRUCTURES, 2016, 143 :63-74
[10]   Compression after impact strength of repaired GFRP composite laminates under repeated impact loading [J].
Andrew, J. Jefferson ;
Arumugam, V. ;
Saravanakumar, K. ;
Dhakal, H. N. ;
Santulli, C. .
COMPOSITE STRUCTURES, 2015, 133 :911-920