摘要
Carbon-carbon composites are widely applied in the area of astronautics and aeronautics. As a kind of advanced composites, its properties are known to depend essentially on the technological regimes of its manufacturing processes. This paper is devoted to the modeling of manufacturing processes of the composites and focuses on establishing the processing-microstructure-property relation to enable design of internal architecture to predict and optimize properties.
源语言 | 英语 |
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页(从-至) | 29-32 |
页数 | 4 |
期刊 | Key Engineering Materials |
卷 | 334-335 I |
出版状态 | 已出版 - 2007 |
已对外发布 | 是 |