The effect of lamina configuration on low-velocity impact behaviour for glass fiber/rubber curved composites

被引:12
作者
Albayrak, Mustafa [1 ,4 ]
Kaman, Mete Onur [2 ]
Bozkurt, Ilyas [3 ]
机构
[1] Inonu Univ, Malatya Organised Ind Zone Vocat Sch, Dept Machine & Met Technol, Malatya, Turkiye
[2] Firat Univ, Engn Fac, Dept Mech Engn, Elazig, Turkiye
[3] Mus Alparslan Univ, Architecture & Engn Fac, Dept Mech Engn, Mus, Turkiye
[4] Inonu Univ, Malatya Organised Ind Zone Vocat Sch, Dept Machine & Met Technol, TR-44900 Malatya, Turkiye
关键词
Curved composites; rubber layer; progressive failure analysis; low-velocity impact; DAMAGE; RUBBER; CARBON; EPOXY; THICKNESS; STRENGTH; PLATES; MODEL; STEEL;
D O I
10.1177/00219983231164950
中图分类号
TB33 [复合材料];
学科分类号
摘要
The aim of this study is to produce curved sandwich composites with different arrays by adding Ethylene Propylene Diene Monomer (EPDM) rubber interlayers between glass fiber woven fabrics and to investigate their behaviours under low-velocity impact. For this purpose, sandwich plates were produced through the vacuum infusion method by using glass fiber and rubber layers on the steel mold manufactured in curved form. Impact tests were applied on the plates and the effect of the stacking sequence for glass fibers/rubber layer on the impact energy absorption was examined. The energy absorption property of the composites was improved by a maximum of 45% with a layer epdm used in the midplane of the composite. Also, when rubber layers were used on the outermost surface of the composites, the damage area reduced by 14%. In the numerical part, the tests were modelled using LS-DYNA finite element packaged programme and the Hashin failure criterion-based material model was used in order to view any damages on the composite structure after the tests. The agreement between numerical and experimental results was obtained with a maximum error of 19%
引用
收藏
页码:1875 / 1907
页数:33
相关论文
共 51 条
[1]   Thermomechanical analysis of antisymmetric laminated reinforced composite plates using a new four variable trigonometric refined plate theory [J].
Abualnour, Moussa ;
Chikh, Abdelbaki ;
Hebali, Habib ;
Kaci, Abdelhakim ;
Tounsi, Abdeldjebbar ;
Bousahla, Abdelmoumen Anis ;
Tounsi, Abdelouahed .
COMPUTERS AND CONCRETE, 2019, 24 (06) :489-498
[2]  
Adachi T, 2017, MECH ENG J, V4, DOI 10.1299/mej.17-00052
[3]  
Albayrak M., 2022, Determination of LS-DYNA MAT162 material input parameters for low velocity impact analysis of layered composites, P39
[4]   Experimental and Computational Analysis of Low-Velocity Impact on Carbon-, Glass- and Mixed-Fiber Composite Plates [J].
AlOmari, Ahmed S. ;
Al-Athel, Khaled S. ;
Arif, Abul Fazal M. ;
Al-Sulaiman, Faleh. A. .
JOURNAL OF COMPOSITES SCIENCE, 2020, 4 (04)
[5]  
[Anonymous], 2015, 10 EUR LS DYNA C 201
[6]   Post impact analysis of damaged variable-stiffness curved composite plates [J].
Arachchige, B. ;
Ghasemnejad, H. .
COMPOSITE STRUCTURES, 2017, 166 :12-21
[7]   Thickness effect on repeated impact response of woven fabric composite plates [J].
Atas, Cesim ;
Icten, Bulent Murat ;
Kucuk, Mumin .
COMPOSITES PART B-ENGINEERING, 2013, 49 :80-85
[8]   Curved sandwich composites with layer-wise graded cores under impact loads [J].
Baba, Buket Okutan .
COMPOSITE STRUCTURES, 2017, 159 :1-11
[9]   Low-velocity impact on cylindrically curved bilayers [J].
Bidi, A. ;
Liaghat, Gh ;
Rahimi, Gh .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART K-JOURNAL OF MULTI-BODY DYNAMICS, 2018, 232 (04) :568-576
[10]   Low velocity impact response of fabric reinforced hybrid composites with stratified filled epoxy matrix [J].
Bunea, M. ;
Circiumaru, A. ;
Buciumeanu, M. ;
Birsan, I. G. ;
Silva, F. S. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2019, 169 :242-248