摘要
Plane-stress constitutive relations for laminate composites undergoing matrix cracking are developed that can be fit to data from uniaxial tests. The constitutive equations are specialized to brittle-matrix composites in the form of cross-plies and quasi-isotropic laminates. The effect of nonlinear stress-strain behavior on stress redistribution around holes and notches in laminate plates is illustrated.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 1245-1255 |
| 页数 | 11 |
| 期刊 | Journal of the American Ceramic Society |
| 卷 | 80 |
| 期 | 5 |
| DOI | |
| 出版状态 | 已出版 - 5月 1997 |
| 已对外发布 | 是 |
学术指纹
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