期刊
COMPOSITES PART B-ENGINEERING
卷 45, 期 1, 页码 1156-1163出版社
ELSEVIER SCI LTD
DOI: 10.1016/j.compositesb.2012.07.034
关键词
Ceramic-matrix composites (CMCs); Stress concentrations; Damage mechanics; Finite element analysis (FEA); Mechanical testing
资金
- Air Force Research Laboratory, Materials and Manufacturing Directorate (AFRL/RX), WPAFB, Ohio, USA [FA8650-03-C-5228, F33615-01-C-5234]
This paper describes a mechanistic modeling approach that attempts to capture the dominant micromechanical deformation and damage mechanisms in woven composites over the temperature and stress ranges relevant to gas turbine engine components. The model is incorporated into a finite-element framework and applied to analyze stress concentration at holes. The materials considered in this study are two-dimensional woven SiC/SiC and SiC/MAS composites. The results include the strain field near circular holes and global load-displacement behavior of the structure. In each case, the model predictions are compared with experimental measurements. Based on these comparisons, conclusions are drawn regarding the efficacy of the modeling approach and needs for further investigations are identified. (c) 2012 Elsevier Ltd. All rights reserved.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据