摘要
The present paper is concerned with the evaluation of microstructure and interior defects of hybrid carbon-carbon composites with increasing temperature. The fracture mechanism of hybrid carbon-carbon composites is also investigated from SEM photographs of fractured surfaces of specimens experienced ultra-high temperature under tensile load, the conclusion is therefore obtained that the porous and cracks coalescence, growth and propagation and the fiber/matrix interfaces degeneration under the combination of ultra-high temperature and load cause strength descend, composite would fractured from a weak section.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 16-21+30 |
| 期刊 | Hangkong Cailiao Xuebao/Journal of Aeronautical Materials |
| 卷 | 22 |
| 期 | 1 |
| 出版状态 | 已出版 - 3月 2002 |
| 已对外发布 | 是 |
指纹
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Yi, F. J., Liang, J., Meng, S. H., & Du, S. Y. (2002). Research on tensile fracture mechanism of hybrid carbon-carbon composites at ultra high temperature. Hangkong Cailiao Xuebao/Journal of Aeronautical Materials, 22(1), 16-21+30.