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
  • [21] Delamination Effect on Bending Behaviour in Carbon-Epoxy Composites
    Amaro, A. M.
    Reis, P. N. B.
    de Moura, M. F. S. F.
    STRAIN, 2011, 47 (02) : 203 - 208
  • [22] In-plane mechanical properties of a carbon-epoxy composite laminate at elevated temperatures
    Zhou, Z. Q.
    Liu, X. L.
    Chiu, W. K.
    POLYMERS & POLYMER COMPOSITES, 2007, 15 (03): : 207 - 216
  • [23] Evaluation of repeated low energy impact damage in carbon-epoxy composite materials
    de Morais, WA
    Monteiro, SN
    d'Almeida, JRM
    COMPOSITE STRUCTURES, 2005, 67 (03) : 307 - 315
  • [24] IMPACT BEHAVIOUR OF HYBRID GLASS/CARBON EPOXY COMPOSITES
    Perez-Martin, M. J.
    Enfedaque, A.
    Dickson, W.
    Galvez, F.
    27TH INTERNATIONAL SYMPOSIUM ON BALLISTICS, VOLS. 1 AND 2, 2013, : 1146 - 1149
  • [25] Low Energy Impact Indentation of an Epoxy-Carbon Fiber Laminate
    Martinez, A. B.
    Xiang, G.
    Arencon, D.
    Velasco, J. I.
    POLYMERS & POLYMER COMPOSITES, 2011, 19 (07): : 553 - 557
  • [26] INVESTIGATION OF THE TRANSVERSE PROPERTIES OF A UNIDIRECTIONAL CARBON-EPOXY LAMINATE .1. MATRIX PROPERTIES
    REZAIFARD, AH
    BADER, MG
    SMITH, PA
    COMPOSITES SCIENCE AND TECHNOLOGY, 1994, 52 (02) : 275 - 285
  • [27] Numerical analysis of low-velocity impact of carbon-basalt/epoxy hybrid laminates
    Maper, Ater
    Karuppanan, Saravanan
    Patil, Santosh S.
    INDIAN JOURNAL OF ENGINEERING AND MATERIALS SCIENCES, 2019, 26 (5-6) : 349 - 355
  • [28] Low velocity impact behaviour of surface treated glass fibre reinforced epoxy matrix hybrid composites
    Sohail, K. S. Mohammed
    Karungaran, N.
    Jeffrey, J. Allen
    MATERIALS TODAY-PROCEEDINGS, 2022, 51 : 1038 - 1041
  • [29] Improvements in the thermomechanical and electrical behavior of hybrid carbon-epoxy nanocomposites
    Lopez-Barroso, J.
    Martinez-Hernandez, A. L.
    Rivera-Armenta, J. L.
    Almendarez-Camarillo, A.
    Garcia-Casillas, P. E.
    Flores-Hernandez, C. G.
    Velasco-Santos, C.
    CARBON TRENDS, 2021, 5
  • [30] Low-velocity impact response characterization of a hybrid titanium composite laminate
    Bernhardt, S.
    Ramulu, M.
    Kobayashi, A. S.
    Proceedings of the ASME Materials Division, 2005, 100 : 203 - 211