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

被引:10
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
    Abualnour, Moussa
    Chikh, Abdelbaki
    Hebali, Habib
    Kaci, Abdelhakim
    Tounsi, Abdeldjebbar
    Bousahla, Abdelmoumen Anis
    Tounsi, Abdelouahed
    [J]. COMPUTERS AND CONCRETE, 2019, 24 (06) : 489 - 498
  • [2] Adachi T, 2017, MECH ENG J, V4, DOI 10.1299/mej.17-00052
  • [3] Albayrak, 2022, DETERMINATION LS DYN, P39
  • [4] Experimental and Computational Analysis of Low-Velocity Impact on Carbon-, Glass- and Mixed-Fiber Composite Plates
    AlOmari, Ahmed S.
    Al-Athel, Khaled S.
    Arif, Abul Fazal M.
    Al-Sulaiman, Faleh. A.
    [J]. JOURNAL OF COMPOSITES SCIENCE, 2020, 4 (04):
  • [5] Post impact analysis of damaged variable-stiffness curved composite plates
    Arachchige, B.
    Ghasemnejad, H.
    [J]. COMPOSITE STRUCTURES, 2017, 166 : 12 - 21
  • [6] Thickness effect on repeated impact response of woven fabric composite plates
    Atas, Cesim
    Icten, Bulent Murat
    Kucuk, Mumin
    [J]. COMPOSITES PART B-ENGINEERING, 2013, 49 : 80 - 85
  • [7] Curved sandwich composites with layer-wise graded cores under impact loads
    Baba, Buket Okutan
    [J]. COMPOSITE STRUCTURES, 2017, 159 : 1 - 11
  • [8] Low-velocity impact on cylindrically curved bilayers
    Bidi, A.
    Liaghat, Gh
    Rahimi, Gh
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART K-JOURNAL OF MULTI-BODY DYNAMICS, 2018, 232 (04) : 568 - 576
  • [9] Low velocity impact response of fabric reinforced hybrid composites with stratified filled epoxy matrix
    Bunea, M.
    Circiumaru, A.
    Buciumeanu, M.
    Birsan, I. G.
    Silva, F. S.
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2019, 169 : 242 - 248
  • [10] Geometrically nonlinear transient analysis of composite laminated plate and shells subjected to low-velocity impact
    Choi, I. H.
    [J]. COMPOSITE STRUCTURES, 2016, 142 : 7 - 14