Effect of ply misalignment on the notched strength of composite laminates

被引:0
|
作者
Vallmajo, O. [1 ]
Descamps, M. [1 ]
Arteiro, A. [2 ,3 ]
Turon, A. [1 ]
机构
[1] Univ Girona, Polytech Sch, AMADE, C-Univ Girona 4, Girona 17003, Spain
[2] Univ Porto, Fac Engn, DEMec, Rua Dr Roberto Frias, P-4200465 Porto, Portugal
[3] INEGI, Rua Dr Roberto Frias 400, P-4200465 Porto, Portugal
关键词
Composites; Ply deviation; Open hole strength; Multi-fidelity; Finite fracture mechanics; Finite element model; PREDICTION; MODEL; DEFORMATION; VARIABILITY;
D O I
10.1016/j.compstruct.2024.118589
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Predicting the notched strength of carbon fiber-reinforced polymers is a crucial aspect of composite structure design, particularly when considering the uncertainties stemming from geometric features, material variability and defects. This study focuses on the influence of ply misalignment at the meso-scale level. The research employs a comprehensive methodology to establish notched strength allowables, integrating analytical (low fidelity), which have limitations in the representation of stacking sequence effects and in the generation of ply misalignments, and computational tools (high fidelity), employing a finite element model (FEM). The investigation emphasizes the need for a holistic understanding of these factors to enhance the accuracy of predictions. The results predicted by the analytical and, specially, the numerical models are in good agreement with experimental results. Both models underscore the decrease of the notched strength due to ply misalignment. Finally, a hybrid approach is proposed given that FEM predictions offer more accuracy and a detailed comprehension of the failure mechanisms, while fast analytical models can be used to propagate the uncertainties and to determine the allowables.
引用
收藏
页数:12
相关论文
共 50 条
  • [41] Notched tensile strength of randomly oriented E-glass composite laminates
    Govindan Potti, P.K.
    Nageswara Rao, B.
    Srivastava, V.K.
    Materials Science and Engineering A, 2000, 282 (01) : 59 - 66
  • [42] THE PREDICTION OF R-CURVES AND NOTCHED TENSILE-STRENGTH FOR COMPOSITE LAMINATES
    WELLS, JK
    BEAUMONT, PWR
    JOURNAL OF MATERIALS SCIENCE, 1987, 22 (04) : 1457 - 1468
  • [43] A CDM-based failure model for predicting strength of notched composite laminates
    Maa, RH
    Cheng, JH
    COMPOSITES PART B-ENGINEERING, 2002, 33 (06) : 479 - 489
  • [44] ON THE PREDICTION OF RESIDUAL STRENGTH FOR NOTCHED LAMINATES
    CAPRINO, G
    JOURNAL OF MATERIALS SCIENCE, 1983, 18 (08) : 2269 - 2273
  • [45] Effect of ply thickness and ply level hybridization on the compression after impact strength of thin laminates
    Sasikumar, A.
    Trias, D.
    Costa, J.
    Blanco, N.
    Orr, J.
    Linde, P.
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2019, 121 : 232 - 243
  • [46] Notched tensile strength of randomly oriented E-glass composite laminates
    Potti, PKG
    Rao, BN
    Srivastava, VK
    MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2000, 282 (1-2): : 59 - 66
  • [47] Estimate of compressive strength of an unidirectional composite lamina using cross-ply and angle-ply laminates
    Scafe, M.
    Raiteri, G.
    Brentari, A.
    Dlacic, R.
    Troiani, E.
    Falaschetti, M. P.
    Besseghini, E.
    FRATTURA ED INTEGRITA STRUTTURALE, 2014, (29): : 399 - 409
  • [48] FATIGUE DAMAGE IN NOTCHED COMPOSITE LAMINATES
    KULKARNI, SV
    MCLAUGHLIN, PV
    MATERIALS SCIENCE AND ENGINEERING, 1977, 30 (02): : 113 - 120
  • [49] Evaluation of a damage-mechanics approach to the modelling of notched strength in KFRP and GRP cross-ply laminates
    Dimant, RA
    Shercliff, HR
    Beaumont, PWR
    COMPOSITES SCIENCE AND TECHNOLOGY, 2002, 62 (02) : 255 - 263
  • [50] EFFECT OF CURING STRESSES ON THE FIRST PLY-FAILURE IN COMPOSITE LAMINATES
    KIM, RY
    HAHN, HT
    JOURNAL OF COMPOSITE MATERIALS, 1979, 13 (JAN) : 2 - 16