Full-field deformation and failure analysis for compression after impact of carbon fibre reinforced polymer laminates

被引:2
|
作者
Dondish, A. [1 ]
Li, L. [2 ]
Melenka, G. W. [1 ]
机构
[1] York Univ, Lassonde Sch Engn, Dept Mech Engn, N York, ON, Canada
[2] Natl Res Council Canada, Aerosp Res Ctr, Ottawa, ON, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
Compression after impact; Carbon fibre reinforced polymer; Digital image correlation; High-speed imaging; MECHANICAL-PROPERTIES; COMPOSITES; CFRP; CAMERA; STRENGTH; PANELS;
D O I
10.1016/j.compstruct.2023.117469
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Residual compressive strength after impact is a critical design factor in assessing damage tolerance of carbon fibre-reinforced polymers (CFRP) for structural applications in aircraft. This study investigated compression after impact (CAI) performance of quasi-isotropic CFRP laminates by measuring 3D deformation and strain using three-dimensional digital image correlation (3D DIC). Before the CAI, these test panels were subjected to dropweight impact testing with energy levels representing visible impact damage (VID). During the CAI testing, deformation behaviours throughout the full loading sequence were captured by twin-camera imaging systems at the front and back faces of panels at standard speed. A single-camera high-speed imaging system captured ultimate failure behaviours at the sample front face. The single-camera high-speed system used four planar mirrors to achieve 3D DIC measurements. This study investigated the effect of boundary conditions on the compressive behaviours of the test panels, where the effect of additional support plates at the front and back surfaces to reduce the unsupported area was compared with the boundary condition of standard anti-buckling guides. The panels with added supports were found to experience deformations dominated by local buckling and final out-ofplane displacements in an S-shaped profile. These panels also exhibited residual strength reductions correlating to impact damage levels and ultimate failure initiating at the damaged region and propagating rapidly along the transverse axis. In comparison, the panels without added supports exhibited failure dominated by global buckling as manifested by large out-of-plane displacements, which had an arc-shaped profile. The DIC measurements were compared against those of mounted biaxial strain gauges. The single-camera high-speed system was shown not only to be feasible for high strain rate testing applications; it also offered a significant cost saving compared to an equivalent twin-camera high-speed system.
引用
收藏
页数:17
相关论文
共 50 条
  • [31] Characterization of progressive damage behaviour and failure mechanism of carbon fibre reinforced DP590 laminates
    Hu, Haichao
    Hu, Ning
    Wei, Qiang
    Liu, Boya
    Wu, Jin
    Wang, Zhanhui
    Yang, Chen
    THIN-WALLED STRUCTURES, 2021, 168
  • [32] Age Deformation After Stamping of Carbon Fiber Reinforced Polycarbonate Laminates
    Nakada, Masayuki
    Ozaki, Hiroaki
    Miyano, Yasushi
    MECHANICS OF COMPOSITE AND MULTIFUNCTIONAL MATERIALS, VOL 7, 2016, : 377 - 385
  • [33] Experimental characterization and numerical study on the interlaminar fracture toughness of carbon fibre reinforced polymer laminates reinforced with carbon nanotubes
    Kumar, M.
    Kumar, P.
    Bhadauria, S. S.
    MATERIALWISSENSCHAFT UND WERKSTOFFTECHNIK, 2022, 53 (12) : 1561 - 1574
  • [34] Multi-axial damage and failure of medical grade carbon fibre reinforced PEEK laminates: Experimental testing and computational modelling
    Gallagher, Elizabeth Anne
    Lamoriniere, Steven
    McGarry, Patrick
    JOURNAL OF THE MECHANICAL BEHAVIOR OF BIOMEDICAL MATERIALS, 2018, 82 : 154 - 167
  • [35] Compression and buckling analysis of 3D printed carbon fibre-reinforced polymer cellular composite structures
    Peng, Chenxi
    Tran, Phuong
    Mouritz, Adrian P.
    COMPOSITE STRUCTURES, 2022, 300
  • [36] Thermal analysis of carbon fibre reinforced polymer decomposition
    Yatim, Norazlina Mohamad
    Shamsudin, Zurina
    Shaaban, Azizah
    Sani, Nurhernida Abdullah
    Jumaidin, Ridhwan
    Shariff, Emy Aqila
    MATERIALS RESEARCH EXPRESS, 2020, 7 (01)
  • [37] Study on impact performances of scarf-repaired carbon fiber reinforced polymer laminates
    Liu Shufeng
    Cheng Xiaoquan
    Xu Yunyan
    Bao Jianwen
    Guo Xin
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2015, 34 (01) : 60 - 71
  • [38] Failure analysis of CFRP laminates subjected to compression after impact: FE simulation using discrete interface elements
    Rivallant, Samuel
    Bouvet, Christophe
    Hongkarnjanakul, Natthawat
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2013, 55 : 83 - 93
  • [39] Effect of Thermal Ageing on the Impact Damage Resistance and Tolerance of Carbon-Fibre-Reinforced Epoxy Laminates
    Garcia-Moreno, Irene
    Angel Caminero, Miguel
    Patricia Rodriguez, Gloria
    Jose Lopez-Cela, Juan
    POLYMERS, 2019, 11 (01)
  • [40] Interlaminar Fracture Toughness of Carbon Fibre-Reinforced Polymer Laminates With Nano- and Micro-Fillers
    Kostopoulos, V.
    Karapappas, P.
    Loutas, T.
    Vavouliotis, A.
    Paipetis, A.
    Tsotra, P.
    STRAIN, 2011, 47 : E269 - E282