A Study on Coupled Field Analysis of 3-D Gas Turbine Blade

3차원 가스터빈 블레이드의 연성 해석에 관한 연구

  • 박근형 (충남대학교 대학원 기계공학과) ;
  • 민택기 (충남대학교 기계공학과) ;
  • 박창수 (조선대학교 대학원 생산가공공학과)
  • Published : 2006.04.01

Abstract

A turbine blade operates under high temperature, high pressure, and the loads have the characteristics that the amplitudes change. Therefore, it is important to perform a stress analysis considering thermal and pressure loads. The purpose of this study is to investigate the effects of these loads on gas turbine blade through thermal stress analysis. The analysis results shows that pressure in gas fluid flow around blade is high in leading edge part, Gas temperature is connections with pressure of flow around blade. The distribution of stress from blade is appearing as is different at suction side and pressure side.

Keywords

References

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