Low velocity impact behaviour of a hybrid carbon-epoxy/cork laminate

被引：8
|
作者：
Silva, F. G. A. [1 ,2 ]
de Moura, M. F. S. F. [2 ]
Magalhaes, A. G. [3 ]
机构：
[1] INEGI Inst Engn Mecan & Gestao Ind, Rua Dr Roberto Frias 400, P-4200465 Oporto, Portugal
[2] Univ Porto, FEUP, DEMec, Rua Dr Roberto Frias, P-4200465 Oporto, Portugal
[3] ISEP, Rua Dr Antonio Bernardino de Almeida 431, P-4200072 Oporto, Portugal
来源：
STRAIN | 2017年 / 53卷 / 06期
关键词：
carbon-epoxy laminates; cohesive zone modelling; cork; hybrid; impact behaviour; COMPOSITES; CORK;
D O I：
10.1111/str.12241
中图分类号：
TB3 [工程材料学];
学科分类号：
0805 ; 080502 ;
摘要：
This work addresses low velocity impact behaviour of monolithic cross-ply carbon-epoxy and hybrid carbon-epoxy/cork laminates. The [0(4), 90(4)](s) layup was selected due to its high mismatch bending between different oriented layers, which is a critical aspect concerning large delamination development at these critical interfaces. The effect of a cork layer inserted at the most critical interface on low velocity impact behaviour of the carbon-epoxy laminate is discussed. Impact response and resulting damage profiles of monolithic and hybrid laminates are compared, and advantages of the hybrid solution are underlined. A numerical analysis including cohesive zone modelling was also performed to assess the damage profiles obtained for the two laminates analysed. The model revealed to be effective for a better comprehension of damage mechanism for both studied cases.
引用
收藏
页数：9
相关论文
共 50 条
  • [31] Low-velocity impact response characterization of a hybrid titanium composite laminate
    Bernhardt, S.
    Ramulu, M.
    Kobayashi, A. S.
    JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 2007, 129 (02): : 220 - 226
  • [32] Prediction of low velocity impact damage in carbon/epoxy laminates
    Xu, S.
    Chen, P. H.
    7TH ASIAN-PACIFIC CONFERENCE ON AEROSPACE TECHNOLOGY AND SCIENCE, APCATS 2013, 2013, 67 : 489 - 496
  • [33] Low velocity impact and pseudo-ductile behaviour of carbon/glass/epoxy and carbon/glass/PMMA hybrid composite laminates for aircraft application at service temperature
    Subadra, Sharath P.
    Griskevicius, Paulius
    Yousef, Samy
    POLYMER TESTING, 2020, 89
  • [34] Buckling Behaviour of Carbon-Epoxy Adhesively-Bonded Scarf Repairs
    Campilho, R. D. S. G.
    de Moura, M. F. S. F.
    Ramantani, D. A.
    Morais, J. J. L.
    Domingues, J. J. M. S.
    JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2009, 23 (10-11) : 1493 - 1513
  • [35] Low-velocity impact behaviour of woven laminate plates with fire retardant resin
    Grasso, Marzio
    Xu, Yigeng
    Ramji, Amit
    Zhou, Gang
    Chrysanthou, Andreas
    Haritos, George
    Chen, Yong
    COMPOSITES PART B-ENGINEERING, 2019, 171 : 1 - 8
  • [36] Numerical investigation on damage behaviour of circular composite laminate under low velocity impact
    Ghosh, Pritam
    Ramajeyathilagam, K.
    MATERIALS TODAY-PROCEEDINGS, 2020, 33 : 5448 - 5454
  • [37] Quantitative validation of carbon-fiber laminate low velocity impact simulations
    English, Shawn A.
    Briggs, Timothy M.
    Nelson, Stacy M.
    COMPOSITE STRUCTURES, 2016, 135 : 250 - 261
  • [38] Suitability Study of Jute-Epoxy Composite Laminate for Low and High Velocity Impact Applications
    Mahesh, Vishwas
    Joladarashi, Sharnappa
    Kulkarni, Satyabodh M.
    ADVANCES IN MECHANICAL DESIGN, MATERIALS AND MANUFACTURE, 2018, 1943
  • [39] Experimental Investigation of Glass-Carbon/Epoxy Hybrid Composites Subjected to Low Velocity Impact Test
    Venkategowda, C.
    Rajanna, S.
    Udupa, N. G. S.
    Keshavamurthy, R.
    FME TRANSACTIONS, 2018, 46 (04): : 595 - 602
  • [40] EFFECT OF INTERLEAVING ON THE IMPACT RESPONSE OF A UNIDIRECTIONAL CARBON-EPOXY COMPOSITE
    LU, WH
    LIAO, FS
    SU, AC
    KAO, PW
    HSU, TJ
    COMPOSITES, 1995, 26 (03): : 215 - 222
12345