中国航空学报(英文版)2024,Vol.37Issue(1) :138-152.DOI:10.1016/j.cja.2023.06.038

Thermodynamic property of sandwich cylindrical shell structure with metallic wire mesh:Numerical modeling and experimental analysis

Xin XUE Guojian SHEN Juan LIAO
中国航空学报(英文版)2024,Vol.37Issue(1) :138-152.DOI:10.1016/j.cja.2023.06.038

Thermodynamic property of sandwich cylindrical shell structure with metallic wire mesh:Numerical modeling and experimental analysis

Xin XUE 1Guojian SHEN 2Juan LIAO1
扫码查看

作者信息

  • 1. Institute of Metal Rubber & Vibration Noise,School of Mechanical Engineering and Automation,Fuzhou University,Fuzhou 350116,China
  • 2. Institute of Metal Rubber & Vibration Noise,School of Mechanical Engineering and Automation,Fuzhou University,Fuzhou 350116,China;Fujian Shuikou Power Generation Group Co.,LTD,Fuzhou 350000,China
  • 折叠

Abstract

As a new addition to lightweight composite structures,the sandwich cylindrical shell with a metallic wire mesh core has emerged as a promising solution for thermodynamic perfor-mance analysis at elevated temperatures.The intricate interwoven cellular formations within the metallic wire mesh pose difficulties for thermo-mechanical modeling and property evaluation.First,the constitutive models employed to characterize hysteresis phenomena were presented,comprising isotropic elasticity,Bergstrom-Boyce model,Ogden hyper-elasticity,and parameter identification through mechanical examinations at varying temperatures.Second,the finite element modeling of cylindrical shell structures was determined for modal and steady-state dynamic analyses.Third,the experimental procedures were carried out,including the preparation of the sandwich cylindrical shell and the dynamic testing platform.The first-order natural frequency of the cylindrical shell structure is close to the resonance frequency of the dynamic test results,with a maximum error of 6.5%,demonstrating the accuracy of the simulation model.When compared to the solid-core cylindrical shell,the average insertion loss of the sandwich cylindrical shell structure within the fre-quency range of 10-1000 Hz at room temperature is up to 11.09 dB.Furthermore,at elevated tem-peratures,the average insertion loss of the sandwich cylindrical shell decreases but fluctuates as the temperature changes.

Key words

Energy dissipation/Metallic matrix composites/Numerical analysis/Sandwich structure/Thermodynamic properties

引用本文复制引用

基金项目

National Natural Science Foundation of China(12272094)

Key Project of National Defence Innovation Zone of Science and Technology Commission of CMC,China(XXX-033-01)

Natural Science Foundation of Fujian Province of China(2022J01541)

出版年

2024
中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
参考文献量33
段落导航相关论文