Virtual testing of realistic aerospace composite structures

被引:0
|
作者
G. A. O. Davies
J. Ankersen
机构
[1] Imperial College,Department of Aeronautics
来源
Journal of Materials Science | 2008年 / 43卷
关键词
Energy Release Rate; Crack Front; Interface Element; Strain Energy Release; Local Stress Concentration;
D O I
暂无
中图分类号
学科分类号
摘要
The feasibility of using simulation of component tests to failure is examined from the view of using this as a design tool to reduce time and costs for future aircraft designs. All aspects are considered, that is modelling correctly the physics of failure mechanisms, having an acceptable CPU time, and ease of interfacing with existing CAE systems for generating models and processing the results. By looking at many benchmarks (including an industrial component) with experimental validation, it is concluded that simulation is now a feasible design tool and that many more searching examples will lend credibility to this strategy for both manufacturers and certification authorities.
引用
收藏
页码:6586 / 6592
页数:6
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