4.7 Article

Size-dependency of the transverse-tensile failure behavior for triaxially braided composites

期刊

COMPOSITES SCIENCE AND TECHNOLOGY
卷 206, 期 -, 页码 -

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.compscitech.2021.108672

关键词

Triaxially braided composite; Free-edge effect; Size dependency; Progressive failure behavior; Meso-scale model

资金

  1. National Natural Science Foundation of China
  2. NSFC [11772267, 12002111]
  3. China Postdoctoral Science Foundation [2020M681101]
  4. 111 Project [BP0719007]
  5. Shaanxi Key Research and Development Program for International Cooperation and Exchanges [2019 KW-020]

向作者/读者索取更多资源

The study investigates the size-dependent failure behavior of single-layer triaxially braided composites under transverse tension load. Experimental and numerical results show a transition in the failure mechanism from fiber bundle pull-out dominated to fiber bundle shear dominated as specimen width increases. Numerical simulation results reveal the correlation of free-edge effect with progressive failure behavior.
Coupon specimens of triaxially braided composites suffer significant out-of-plane tension-torsion coupled deformation along the free edges, known as free-edge effect, under uniaxial tensile/compressive loading. The presence of free-edge effect causes variations in the measured stiffness and strength properties with specimen size. In this study, the size-dependent failure behavior of a single-layer triaxially braided composite under transverse tension load is investigated. Experiments are conducted to characterize the stress-strain response and failure pattern of straight-sided coupon specimens with various widths. Digital image correlation is used to monitor the free-edge-effect-induced tension-torsion coupled deformation. An improved meso-scale finite element model is developed to enable simulation of fiber bundle pull-out failure by introducing a fully covered tow-to-tow interface and plastic failure of the pure matrix zone. The model captures the size-dependent stress-strain response, free-edge effect induced premature failure and ultimate failure phenomena of the braided composite. The experimental and numerical results identify the transition of the failure mechanism from one that is dominated by fiber bundle pull-out to one that is dominated by fiber bundle shear as the specimen width is increased. The numerical simulation results reveal the correlation of free-edge effect with the progressive failure behavior, and they aid in identifying the major stress components that are contributing to the failure. The conclusions provide useful insights for the structural design and architecture optimization of triaxially braided composites.

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