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基于径轴向Tchebichef矩函数三维曲面非对称结构的模型修正

张浩 臧朝平

张浩, 臧朝平. 基于径轴向Tchebichef矩函数三维曲面非对称结构的模型修正[J]. 航空动力学报, 2020, 35(10): 2205-2215. doi: 10.13224/j.cnki.jasp.2020.10.021
引用本文: 张浩, 臧朝平. 基于径轴向Tchebichef矩函数三维曲面非对称结构的模型修正[J]. 航空动力学报, 2020, 35(10): 2205-2215. doi: 10.13224/j.cnki.jasp.2020.10.021
ZHANG Hao, ZANG Chaoping. Model validation of three-dimensional curved asymmetric structure by radial axial Tchebichef moments[J]. Journal of Aerospace Power, 2020, 35(10): 2205-2215. doi: 10.13224/j.cnki.jasp.2020.10.021
Citation: ZHANG Hao, ZANG Chaoping. Model validation of three-dimensional curved asymmetric structure by radial axial Tchebichef moments[J]. Journal of Aerospace Power, 2020, 35(10): 2205-2215. doi: 10.13224/j.cnki.jasp.2020.10.021

基于径轴向Tchebichef矩函数三维曲面非对称结构的模型修正

doi: 10.13224/j.cnki.jasp.2020.10.021
基金项目: 国家自然科学基金(11372128)

Model validation of three-dimensional curved asymmetric structure by radial axial Tchebichef moments

  • 摘要: 采用积分的思想,将曲面机匣看作由若干圆柱机匣积累而成,将曲面机匣振型数据插值到一个圈数×点数×层数的三维像素空间内,能够实现径轴向Tchebichef矩(RAT矩)对曲面机匣模态振型的识别。利用RAT矩函数从曲面结构模态振型数据提取矩特征值,实现对振型数据的压缩,基于矩特征值的相关性分析能够很好地描述重模态现象,弥补了传统模态置信准则(MAC)值对于重模态描述的缺陷。进而将矩特征值代替振型数据,作为目标函数,应用于模型修正。矩特征值的数据量远小于振型数据,能够提高计算效率、避免修正结果不收敛。考虑到工程部件大多非完全轴对称,以一个带有非对称凸台的航空发动机机匣为例,基于RAT矩进行模态计算、相关分析和模型修正,发现同时利用频率与RAT矩进行模型修正,相关性有明显的提升,例如第9阶模态的相关性由35.35%提升到67.21%。各阶模态对的频差也都明显降低,最大频差由14.56%降至9.09%。证明了RAT矩函数能够应用在三维曲面非对称机匣的模型确认中。

     

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出版历程
  • 收稿日期:  2020-01-03
  • 刊出日期:  2020-10-28

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