摘要
Morphology and mechanical properties of clay/high-functional epoxy nanocomposites are investigated. An intercalated morphology is always observed for clay loadings ≤5 wt %. The glass transition temperature (Tg) of the composites decreases with the clay loading, and the impact strength increases first by 10% at 2 wt% clay loading, and is followed by a dramatic decline, while the flexural strength decreases in all cases.
源语言 | 英语 |
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页(从-至) | 279-282 |
页数 | 4 |
期刊 | Chinese Journal of Aeronautics |
卷 | 18 |
期 | 3 |
DOI | |
出版状态 | 已出版 - 8月 2005 |