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基于高保真有限元模型失谐叶盘受迫响应的统计特性

张秉杰 臧朝平 PETROV E P

张秉杰, 臧朝平, PETROV E P. 基于高保真有限元模型失谐叶盘受迫响应的统计特性[J]. 航空动力学报, 2019, 34(1): 135-141. doi: 10.13224/j.cnki.jasp.2019.01.016
引用本文: 张秉杰, 臧朝平, PETROV E P. 基于高保真有限元模型失谐叶盘受迫响应的统计特性[J]. 航空动力学报, 2019, 34(1): 135-141. doi: 10.13224/j.cnki.jasp.2019.01.016
Statistical characteristics of forced response in mistuned bladed disks based on high-fidelity finite element model[J]. Journal of Aerospace Power, 2019, 34(1): 135-141. doi: 10.13224/j.cnki.jasp.2019.01.016
Citation: Statistical characteristics of forced response in mistuned bladed disks based on high-fidelity finite element model[J]. Journal of Aerospace Power, 2019, 34(1): 135-141. doi: 10.13224/j.cnki.jasp.2019.01.016

基于高保真有限元模型失谐叶盘受迫响应的统计特性

doi: 10.13224/j.cnki.jasp.2019.01.016
基金项目: 国家自然科学基金(11372128);国家自然科学基金委员会与中国工程物理研究院联合基金(U1730129)

Statistical characteristics of forced response in mistuned bladed disks based on high-fidelity finite element model

  • 摘要: 采用极值理论分析失谐叶盘最大受迫响应的统计特性并应用于某压气机叶盘上。对失谐叶盘进行减缩建模,运用蒙特卡洛方法模拟响应计算,研究不同激励阶次下最大响应放大因子的分布特性。采用极值理论对最大响应放大因子分布进行统计学建模,以极大似然估计方法求解未知参数,进行分布拟合,并采用K-S(Kolmogorov-Smirnov)检验方法检验各分布函数拟合的好坏程度。对某压气机叶盘进行失谐响应统计特性分析,对比了7种分布函数对最大响应放大因子的拟合效果,结果表明:极值分布、二参数威布尔分布、正态分布、对数正态分布和伽马分布拟合效果较差;常用的三参数威布尔分布不如广义极值分布的拟合效果好。因此,说明广义极值分布更能准确地描述失谐叶盘动力响应的统计特性。

     

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出版历程
  • 收稿日期:  2017-12-07
  • 刊出日期:  2019-01-28

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