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基于热力等效模型的波纹夹芯板热颤振计算

祁武超 翟梦琦

沈阳航空航天大学学报2026,Vol.43Issue(1):1-8,8.
沈阳航空航天大学学报2026,Vol.43Issue(1):1-8,8.DOI:10.3969/j.issn.2095-1248.2026.01.001

基于热力等效模型的波纹夹芯板热颤振计算

Thermal flutter calculation of corrugated sandwich panels based on the thermo-mechanical equivalent model

祁武超 1翟梦琦1

作者信息

  • 1. 沈阳航空航天大学 辽宁省飞行器复合材料结构分析与仿真重点实验室,沈阳 110136
  • 折叠

摘要

Abstract

To efficiently predict the dynamic stability of integrated thermal protection systems under aerodynamic heating environment,a thermal flutter calculation method for corrugated sandwich panels based on a thermo-mechanical equivalent model was proposed,aiming to enhance the computational efficiency of finite element analysis.First,the homogenization theory was applied to approximate the core layer as a single layer of orthotropic material,thereby simplifying the model.Second,the proportion of the areas occupied by the web and the insulating material was redefined to increase the characteristic size of the equivalent area,thereby reducing the number of finite element grids while ensuring the accuracy of the temperature gradient.Finally,based on the developed thermo-mechanical equivalent model,the modal characteristics of the corrugated sandwich panel were extracted,and the p-k method was employed for thermal flutter analysis to evaluate the aerodynamic response.The results show that this method improves computational efficiency by 80%,and the error is controlled within 3%.

关键词

波纹夹芯板/正交各向异性材料/热力等效模型/热颤振/均质化理论

Key words

corrugated sandwich panel/orthotropic material/thermo-mechanical equivalent model/thermal flutter/homogenization theory

分类

航空航天

引用本文复制引用

祁武超,翟梦琦..基于热力等效模型的波纹夹芯板热颤振计算[J].沈阳航空航天大学学报,2026,43(1):1-8,8.

基金项目

辽宁省教育厅面上项目(项目编号:JYTMS20230253,JYTMS20230224). (项目编号:JYTMS20230253,JYTMS20230224)

沈阳航空航天大学学报

2095-1248

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