Equivalent stress concept to account for the effect of local cyclic stress ratio on transverse cracking in tension-tension fatigue

被引:1
作者
Gabriel, Vivek Richards Pakkam [1 ]
Loukil, Mohamed Sahbi [2 ]
Fernberg, Patrik [1 ]
Varna, Janis [1 ,3 ]
机构
[1] Lulea Univ Technol, Dept Engn Sci & Math, SE-97187 Lulea, Sweden
[2] Linkoping Univ, Dept Management & Engn, SE-58183 Linkoping, Sweden
[3] Riga Tech Univ, Lab Expt Mech Mat, LV-1048 Riga, Latvia
基金
瑞典研究理事会;
关键词
Polymer-matrix composites; Fatigue; Transverse cracking; Statistical methods; UNIDIRECTIONAL COMPOSITES; GROWTH-MODEL; MATRIX; EVOLUTION; DAMAGE; PREDICTION; MECHANISM; BEHAVIOR; FRACTURE; RESIN;
D O I
10.1016/j.ijfatigue.2024.108482
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Presented test results on transverse cracking in cross-ply laminates upon tension-tension cyclic loading show that the increase of crack density depends not only on the maximum transverse stress in the cycle but also on the local cyclic stress ratio RlocT in the analyzed layer. To include the effect of the RlocT in the model with statistical failure stress distribution for crack initiation (based on Weibull distribution) adapted for fatigue, an equivalent stress is introduced in a similar manner as the equivalent strain energy release rate has been used for delamination crack propagation. The equivalent stress in the layer is defined as a power function of the maximum stress and the stress ratio in the layer. It was found, testing laminates with two different fiber contents that higher the local stress ratio in 90-layer, higher the transverse cracking resistance. Transverse crack density simulation using the developed equivalent stress model has been validated against test results.
引用
收藏
页数:8
相关论文
共 30 条
  • [1] Delamination growth behavior of a fabric reinforced laminated composite under mode I fatigue
    Atodaria, DR
    Putatunda, SK
    Mallick, PK
    [J]. JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 1999, 121 (03): : 381 - 385
  • [2] A fatigue crack growth model for random fiber composites
    Atodaria, DR
    Putatunda, SK
    Mallick, PK
    [J]. JOURNAL OF COMPOSITE MATERIALS, 1997, 31 (18) : 1838 - 1855
  • [3] Fatigue crack growth model and mechanism of a random fiber SMC composite
    Atodaria, DR
    Putatunda, SK
    Mallick, PK
    [J]. POLYMER COMPOSITES, 1999, 20 (02) : 240 - 249
  • [4] BAILEY JE, 1981, J MATER SCI, V16, P649, DOI 10.1007/BF02402782
  • [5] Prediction of the crack density evolution in multidirectional laminates under fatigue loadings
    Carraro, P. A.
    Maragoni, L.
    Quaresimin, M.
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2017, 145 : 24 - 39
  • [6] Intralaminar cracking during cyclic loading in laminates with distributed failure stress in 90-plies
    Gabriel, Vivek Richards Pakkam
    Loukil, Mohamed Sahbi
    Varna, Janis
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2022, 161
  • [7] Analysis of intralaminar cracking in 90-plies of GF/EP laminates with distributed ply strength
    Gabriel, Vivek Richards Pakkam
    Loukil, Mohamed Sahbi
    Varna, Janis
    [J]. JOURNAL OF COMPOSITE MATERIALS, 2021, 55 (26) : 3925 - 3942
  • [8] Transverse cracking of cross-ply laminates: A computational micromechanics perspective
    Herraez, Miguel
    Mora, Diego
    Naya, Fernando
    Lopes, Claudio S.
    Gonzalez, Carlos
    LLorca, Javier
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2015, 110 : 196 - 204
  • [9] Predicting fatigue transverse crack growth in cross-ply carbon-epoxy laminates from quasi static strength tests by using iso-damage curves
    Hoang, Nguyen The
    Gamby, Denys
    Lafarie-Frenot, Marie-Christine
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2010, 32 (01) : 166 - 173
  • [10] EFFECT OF STRESS RATIO ON NEAR-THRESHOLD PROPAGATION OF DELAMINATION FATIGUE CRACKS IN UNIDIRECTIONAL CFRP
    HOJO, M
    TANAKA, K
    GUSTAFSON, CG
    HAYASHI, R
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 1987, 29 (04) : 273 - 292