...
首页> 外文期刊>Composite Structures >Reliability formulation for composite laminates subjected to first-ply failure
【24h】

Reliability formulation for composite laminates subjected to first-ply failure

机译:经受第一层破坏的复合层压板的可靠性公式

获取原文
获取原文并翻译 | 示例

摘要

Methods formulated on the basis of the concept of first-ply failure and the structural reliability theory are presented for the reliability analysis of laminated composite plates. In the reliability formulation, an appropriate phenomenological failure criterion is used to establish the limit state equation of the laminated composite plates, and different numerical techniques are employed to evaluate the reliability of the plates. Experimental investigations of lamina strengths and first-ply failure loads of laminated composite plates were performed. Baseline probability distributions of lamina strength parameters constructed from the test data are used to study the reliability of the laminated plates. The accuracy of the proposed models in reliability assessment of the laminated plates are verified by the experimental results on first-ply failure load distributions.
机译:提出了基于第一层破坏概念和结构可靠性理论制定的方法,用于复合材料层合板的可靠性分析。在可靠性公式中,使用适当的现象学破坏准则建立层合复合板的极限状态方程,并采用不同的数值技术评估板的可靠性。对层压复合板的层板强度和第一层破坏载荷进行了实验研究。根据测试数据构造的层板强度参数的基线概率分布用于研究层压板的可靠性。通过对第一层破坏载荷分布的实验结果验证了所提出模型在层压板可靠性评估中的准确性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号