摘要
推导了具有随机性时Neumann随机有限元法的基本方程,用级数来拟合结构响应的概率密度函数,并通过数值积分计算结构的可靠度。对涡轮叶片的可靠度分析表明,该方法可利用较小的样本容量获得较高的计算精度,并具有较高的计算效率。
An extended Neumann Stochastic Finite Element Method(NSFEM)has been derived.Probability Density Function(PDF)of blade displacement and stress can be obtained by applying series fitting.Then the numerical integral method is used to compute the reliability of structure.The analysis of two numerical examples shows that the proposed approach is of good computational accuracy and efficiency with a small capacity for samples
出处
《推进技术》
EI
CAS
CSCD
北大核心
1998年第2期35-37,共3页
Journal of Propulsion Technology
关键词
涡轮
叶片
结构可靠性
有限元
航空发动机
Turbine blade,Structural reliability,Neumann problem,Finite element method,Probability density function