TY - JOUR
T1 - Effect of porosity on high-temperature tensile properties of 2D woven C/SiC with hole-edge densification structure
AU - Huang, Sheng
AU - Jiang, Zhuoqun
AU - Rong, Le
AU - Wang, Zhanxue
AU - Tokovyy, Yuriy
N1 - Publisher Copyright:
© 2025
PY - 2025/7
Y1 - 2025/7
N2 - This study proposes a modeling approach that characterizes the hole-edge densification structure of open-hole 2D braided C/SiC composites during chemical vapor infiltration (CVI). An embedded multi-scale progressive damage modeling method is proposed to characterize the densified structure of hole edges·, considering the random distribution of pores. Subsequently, a macro-meso model was established, integrating 2D woven C/SiC composites with hole-edge densification. A high-temperature progressive damage model for 2D braided C/SiC composites was established. The stiffness matrix was modified according to the various damage modes and loading conditions of the fiber and matrix to simulate the nonlinear mechanical behavior of the composites. Compared to the experimental data and the homogenized model, the errors in the macro and micro models can be reduced by 69.1 %. The analysis indicates that the average thermal stress in the matrix and warp increases with rising temperature, while the thermal stress in the weft yarn exhibits minimal variation with temperature changes. When the porosity is below 10 %, the average stress in the dense area near the hole edge remains low. Conversely, when the porosity exceeds 10 %, the average thermal stress in the dense area surpasses that in the non-dense area. The uniaxial tensile strength of 2D braided C/SiC composites with varying porosity initially increases and then decreases with rising temperature. Additionally, at different temperatures, the locations of fracture damage in 2D braided C/SiC composites with different porosities vary.
AB - This study proposes a modeling approach that characterizes the hole-edge densification structure of open-hole 2D braided C/SiC composites during chemical vapor infiltration (CVI). An embedded multi-scale progressive damage modeling method is proposed to characterize the densified structure of hole edges·, considering the random distribution of pores. Subsequently, a macro-meso model was established, integrating 2D woven C/SiC composites with hole-edge densification. A high-temperature progressive damage model for 2D braided C/SiC composites was established. The stiffness matrix was modified according to the various damage modes and loading conditions of the fiber and matrix to simulate the nonlinear mechanical behavior of the composites. Compared to the experimental data and the homogenized model, the errors in the macro and micro models can be reduced by 69.1 %. The analysis indicates that the average thermal stress in the matrix and warp increases with rising temperature, while the thermal stress in the weft yarn exhibits minimal variation with temperature changes. When the porosity is below 10 %, the average stress in the dense area near the hole edge remains low. Conversely, when the porosity exceeds 10 %, the average thermal stress in the dense area surpasses that in the non-dense area. The uniaxial tensile strength of 2D braided C/SiC composites with varying porosity initially increases and then decreases with rising temperature. Additionally, at different temperatures, the locations of fracture damage in 2D braided C/SiC composites with different porosities vary.
KW - 2D braided C/SiC composites
KW - High-temperature tensile properties
KW - Hole edge densification structure
KW - Macro-meso hybrid model
UR - http://www.scopus.com/inward/record.url?scp=105004397820&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2025.110247
DO - 10.1016/j.ast.2025.110247
M3 - 文章
AN - SCOPUS:105004397820
SN - 1270-9638
VL - 162
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 110247
ER -