In-plane thermal expansion behavior of M55J carbon fiber reinforced SiC matrix composite

Dang, Xiaolin; Zhao, Donglin; Fan, Xiaomeng; Ma, Xiaokang; Chen, Xiang; Xue, Jimei; Ye, Fang; Liu, Yongsheng

doi:10.1016/j.jeurceramsoc.2023.08.044

Journal of the European Ceramic Society

2024

DOI: 10.1016/j.jeurceramsoc.2023.08.044

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In-plane thermal expansion behavior of M55J carbon fiber reinforced SiC matrix composite

Xiaolin Dang,

Donglin Zhao,

Xiaomeng Fan

et al.

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Cited by 5 publications

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A method for predicting thermal expansion coefficients of carbon fiber/epoxy composites with void defects

Wang,

Huang,

Shan

et al. 2024

Polymer Composites

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To predict the coefficient of thermal expansion (CTE) of carbon fiber/epoxy resin composites with void defects comprehensively and accurately, a comprehensive study is carried out by integrating experiment, analytical model (ANM), and finite element model (FEM). The experiments on composites are conducted combining with Micro‐CT to provide geometric parameters and verification for ANM and FEM. An ANM considering void defects is established based on the Chamis model to investigate the influence of porosity, temperature and the ratio of modulus of the constituents of composites. A FEM is established to verify the ANM and reveal the mechanisms of the influence of void defects. The results show that the proposed ANM has high agreement with FEM and experiment. The longitudinal CTE decreases by 61.94% as the porosity increases from 0% to 20% at 60°C, and the same change of porosity results in a 15.62% decrease at 180°C. The transverse CTE is less susceptible to changes in porosity, showing reductions of 2.32% at 60°C and 3.33% at 180°C.Highlights An innovative model is proposed to predict CTE considering void defects. The glass transition temperature Tg of the resin has a significant effect on CTE. Void defects change the homogeneity of the original stress field of the matrix. The reduction of the longitudinal CTE caused by void defects is more significant.

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A method for predicting thermal expansion coefficients of carbon fiber/epoxy composites with void defects

Wang,

Huang,

Shan

et al. 2024

Polymer Composites

View full text Add to dashboard Cite

show abstract

3D microstructure characterization of 2D Cf-ZrB2-SiC ultra-high temperature ceramic matrix composites using X-ray microscopy

Ranjan Mishra,

Singh,

Patel

et al. 2024

Ceramics International

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Ablative property and mechanism of pitch-based carbon fiber modified C/C composites with high thermal conductivity

Zhang,

Luo,

Yang

et al. 2024

Ceramics International

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In-plane thermal expansion behavior of M55J carbon fiber reinforced SiC matrix composite

Cited by 5 publications

References 45 publications

A method for predicting thermal expansion coefficients of carbon fiber/epoxy composites with void defects

A method for predicting thermal expansion coefficients of carbon fiber/epoxy composites with void defects

3D microstructure characterization of 2D Cf-ZrB2-SiC ultra-high temperature ceramic matrix composites using X-ray microscopy

Ablative property and mechanism of pitch-based carbon fiber modified C/C composites with high thermal conductivity

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