摘要
Two kinds of new anti-buckling supports for the specimens of the smooth composite laminates and notched composite laminates were designed. The compression-compression fatigue tests of the smooth composite laminates and notched composite laminates were briefly given. The damage mechanism was analyzed and discussed. A transition concept of fatigue damage mechanism was presented.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 99-102 |
| 页数 | 4 |
| 期刊 | Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica |
| 卷 | 15 |
| 期 | 3 |
| 出版状态 | 已出版 - 1998 |
| 已对外发布 | 是 |
指纹
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