Application of the residual strength degradation model to carbon-epoxy composite

被引:0
|
作者
S. Putić
M. Rakin
S. Bošnjak
机构
[1] University of Belgrade,Faculty of Technology and Metallurgy
[2] University of Belgrade,Faculty of Mechanical Engineering
来源
Materials Science | 2008年 / 44卷
关键词
Fatigue; Fatigue Strength; Ultimate Strength; Stress Ratio; Fiber Orientation;
D O I
暂无
中图分类号
学科分类号
摘要
A residual strength degradation model for two orientations of fibers of carbon-epoxy composite is proposed. The model is constructed on the basis of an analysis of a gradual decrease in the residual strength of the composite and an increase in loading cycles. Two groups of specimens were subjected to tensile tests under static and dynamic loading. It was necessary to determine the relationship between static and dynamic properties of the composite to predict the residual strength for different numbers of loading cycles. On the basis of initial experimental results, the values of the parameters obtained by using the model were computed numerically. The statistical distributions of the corresponding ultimate strengths obtained by using the model were compared with the distributions of experimental results, and their good correlation is demonstrated.
引用
收藏
页码:446 / 450
页数:4
相关论文
共 50 条
  • [1] Low-cycle Fatigue of Thermally-Cycled Carbon-Epoxy Composite
    Unigovski, Ya. B.
    Grinberg, A.
    Gutman, E. M.
    Shneck, R.
    JOURNAL OF METALS MATERIALS AND MINERALS, 2012, 22 (01): : 21 - 30
  • [2] Assessment of damage in a unidirectional off-axis carbon-epoxy composite under cyclic loading
    Sorensen, LK
    Plumtree, A
    COMPOSITE MATERIALS: TESTING AND DESIGN, FOURTEENTH VOLUME, 2003, 1436 : 336 - 348
  • [3] DELAMINATION FATIGUE PROPERTIES OF Z-PINNED CARBON-EPOXY LAMINATE USING METAL OR COMPOSITE RODS
    Pegorin, F.
    Pingkarawat, K.
    Daynes, S.
    Mouritz, A. P.
    20TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS, 2015,
  • [4] Study of the phenomenon of fatigue delamination in a carbon-epoxy composite under mixed mode I/II fracture employing an asymmetric specimen
    Rubiera, S.
    Arguelles, A.
    Vina, J.
    Rocandio, C.
    INTERNATIONAL JOURNAL OF FATIGUE, 2018, 114 : 74 - 80
  • [5] Prediction of Stress Intensity Factor on Precracked Composite Wing Rib Made up of Carbon-Epoxy IM7-8552
    Sivakumar V.
    Dani K.P.
    Sriram S.
    Journal of Failure Analysis and Prevention, 2016, 16 (04) : 635 - 646
  • [6] Fatigue residual strength of circular laminate graphite-epoxy composite plates damaged by transverse load
    Minak, G.
    Morelli, P.
    Zucchelli, A.
    COMPOSITES SCIENCE AND TECHNOLOGY, 2009, 69 (09) : 1358 - 1363
  • [7] Residual strength degradation of cross-ply titanium matrix composite due to elevated temperature
    Calcaterra, JR
    Mall, S
    Ruiz, A
    JOURNAL OF COMPOSITES TECHNOLOGY & RESEARCH, 1999, 21 (01): : 16 - 24
  • [8] Adaptive active vibration control to improve the fatigue life of a carbon-epoxy smart structure
    Ripamonti, Francesco
    Cazzulani, Gabriele
    Cinquemani, Simone
    Resta, Ferruccio
    Torti, Alessandro
    ACTIVE AND PASSIVE SMART STRUCTURES AND INTEGRATED SYSTEMS 2015, 2015, 9431
  • [9] Effects of residual stresses on interlaminar radial strength of Glass-Epoxy L-bend composite laminates
    Umarfarooq, M. A.
    Gouda, P. S. Shivakumar
    Bharath, K. N.
    Veereshkumar, G. B.
    Banapurmath, N. R.
    Edacherian, Abhilash
    FRATTURA ED INTEGRITA STRUTTURALE-FRACTURE AND STRUCTURAL INTEGRITY, 2022, 16 (61): : 140 - 153
  • [10] Residual strength degradation model of 18CrNiMo7-6 forged steel
    Wang, Wei
    Li, Jianmin
    Pan, Jun
    Chen, Huanguo
    Qian, Ping
    Chen, Wenhua
    ADVANCES IN MECHANICAL ENGINEERING, 2019, 11 (04)