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Effect of different heat transfer coefficients on the performance of thermal barrier coatings under thermo-mechanical couple process

  • Zhi Yong Li*
  • , Rui Bao
  • , Jian Yu Zhang
  • , Hao Ju Hu
  • , Bin Jun Fei
  • *Corresponding author for this work
  • Beihang University

Research output: Contribution to journalArticlepeer-review

Abstract

The heat insulation and stress distribution in thermal barrier coatings (TBCs) with different inner wall heat transfer coefficients were studied via finite element method (FEM), laying a foundation for the selection of heat transfer coefficients. The results show that, the temperature of model decreases with the increase of the inner wall heat transfer coefficients, meanwhile, the temperature difference between inner and outer walls increases non-linearly. The maximum stress occurs near the thermally grown oxide (TGO) layer, and its value increases with the increase of heat transfer coefficients.

Original languageEnglish
Pages (from-to)946-951
Number of pages6
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume23
Issue number5
StatePublished - May 2008

Keywords

  • Aerospace propulsion system
  • Finite element method (FEM)
  • Heat transfer coefficient
  • Thermal barrier coatings (TBCs)
  • Thermally grown oxide (TGO)

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