Selective ply-level hybridisation for improved notched response of composite laminates

被引:52
作者
Furtado, C. [1 ]
Arteiro, A. [1 ]
Catalanotti, G. [1 ,2 ]
Xavier, J. [2 ,3 ]
Camanho, P. P. [1 ,2 ]
机构
[1] Univ Porto, Fac Engn, DEMec, Rua Dr Roberto Frias S-N, P-4200465 Oporto, Portugal
[2] Inst Ciencia & Inovacao Engn Mecan & Engn, INEGI, Rua Dr Roberto Frias 400, P-4200465 Oporto, Portugal
[3] Univ Tras Os Montes & Alto Douro, CITAB, Engn 1, Apartado 1013, P-5001801 Vila Real, Portugal
关键词
Thin-ply laminates; Hybrid; Mechanical properties; Notched response; TENSILE-STRENGTH; SIZE; FAILURE;
D O I
10.1016/j.compstruct.2016.02.050
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This work presents an experimental study on the effect of ply-level hybridisation on the tensile unnotched and notched response of composite laminates. In a first assessment, notched tests were performed on laminates with nominal ply thicknesses between 0.03 mm and 0.30 mm. From the understanding of the effect of ply thickness on the damage mechanisms that govern the notched response of laminates, the concept of ply-level hybridisation is introduced, which consists in combining plies of different grades. A uniform combination of thin and conventional plies resulted in a hybrid laminate with intermediate notched response. Selective hybridisation, where thin off-axis plies are combined with thicker 0 degrees plies, resulted in a globally enhanced notched behaviour without compromising the unnotched and fatigue responses. This work clearly shows how ply-level hybridisation, when designed to trigger specific damage mechanisms, can be used to improve the notched response of composite laminates. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1 / 14
页数:14
相关论文
共 24 条
[1]   Thin ply composites: Experimental characterization and modeling of size-effects [J].
Amacher, R. ;
Cugnoni, J. ;
Botsis, J. ;
Sorensen, L. ;
Smith, W. ;
Dransfeld, C. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2014, 101 :121-132
[2]   Notched response of non-crimp fabric thin-ply laminates [J].
Arteiro, A. ;
Catalanotti, G. ;
Xavier, J. ;
Camanho, P. P. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2013, 79 :97-114
[3]  
ASTM International West Conshohocken PA USA, 2014, ASTM D3039 D3039M 14
[4]   Prediction of in situ strengths and matrix cracking in composites under transverse tension and in-plane shear [J].
Camanho, PP ;
Dávila, CG ;
Pinho, ST ;
Iannucci, L ;
Robinson, P .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2006, 37 (02) :165-176
[5]   Measurement of the compressive crack resistance curve of composites using the size effect law [J].
Catalanotti, G. ;
Xavier, J. ;
Camanho, P. P. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2014, 56 :300-307
[6]   Speckle pattern quality assessment for digital image correlation [J].
Crammond, G. ;
Boyd, S. W. ;
Dulieu-Barton, J. M. .
OPTICS AND LASERS IN ENGINEERING, 2013, 51 (12) :1368-1378
[7]   Ultra-lightweight carbon fibre/thermoplastic composite material using spread tow technology [J].
EL-Dessouky, Hassan M. ;
Lawrence, Carl A. .
COMPOSITES PART B-ENGINEERING, 2013, 50 :91-97
[8]   Size effects on the tensile and compressive failure of notched composite laminates [J].
Ercin, G. H. ;
Camanho, P. P. ;
Xavier, J. ;
Catalanotti, G. ;
Mandi, S. ;
Linde, P. .
COMPOSITE STRUCTURES, 2013, 96 :736-744
[9]   An experimental investigation into the tensile strength scaling of notched composites [J].
Green, B. G. ;
Wisnom, M. R. ;
Hallett, S. R. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2007, 38 (03) :867-878
[10]   Damage occurrence at edges of non-crimp-fabric thin-ply laminates under off-axis uniaxial loading [J].
Guillamet, G. ;
Turon, A. ;
Costa, J. ;
Renart, J. ;
Linde, P. ;
Mayugo, J. A. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2014, 98 :44-50