THERMOMECHANICAL STRESS-FIELDS IN HIGH-TEMPERATURE FIBROUS COMPOSITES .2. LAMINATED PLATES

被引：4

作者：

DVORAK, GJ ^{[1
]}

CHEN, TY ^{[1
]}

TEPLY, J ^{[1
]}

机构：

[1] ALCOA LABS,ALCOA CTR,PA 15069

来源：

COMPOSITES SCIENCE AND TECHNOLOGY | 1992年 / 43卷 / 04期

关键词：

LAMINATED COMPOSITE PLATES; INITIAL FAILURE MAPS; THERMOMECHANICAL DEFORMATION;

D O I：

10.1016/0266-3538(92)90059-C

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

The results of Part I of this work are extended to laminated plates. It is assumed that the plates are, at most, macroscopically orthotropic, and that they are subjected to a uniform change in temperature and to in-plane mechanical loads. Average stresses and microstress fields are evaluated in each layer of the plate. Failure envelopes based on critical magnitudes of interface and axial matrix stresses are constructed for one of the SiC/Ti-Al-Nb systems of Part I.

引用

页码：359 / 368

页数：10

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