| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 9702434 | Chinese Journal of Aeronautics | 2005 | 4 Pages |
Abstract
Morphology and mechanical properties of clay/high-functional epoxy nanocomposites are investigated. An intercalated morphology is always observed for clay loadings â¤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.
Related Topics
Physical Sciences and Engineering
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Aerospace Engineering
Authors
Feng DAI, Ya-hong XU, Ya-ping ZHENG, Xiao-Su YI,