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Numericla Study on the Aerodynamic Performances of the Turbo Blower Using Fluid-Structure Interaction Method

유체 구조 연계 해석기법을 적용한 터보블로워 공력성능 해석에 관한 수치적 연구

  • 박태규 (경상대학교 기계공학부 대학원) ;
  • 정희택 (경상대학교 기계공학부) ;
  • 김형범 (경상대학교 기계공학부) ;
  • 박준영 (한국기계연구원 에너지플랜트연구본부)
  • Received : 2011.06.28
  • Accepted : 2011.10.06
  • Published : 2011.12.31

Abstract

The present study aims at investigating the effect of the fluid-structure interaction on the aerodynamic performances in the turbo blower. The design specifications of the reference model driven by 400kW power were given as 7.43kg/s of mass flow rate, 1.66 of pressure ratio with 12000rpm of impeller rotating speed. Numerical simulation has been performed on the three cases based on the tip clearance between the impeller blade and the shroud. The CFX-turbo for flow fields and ANSYS-mechanical for structure domain were applied to solve the present FSI problems inside the turbo blower. Through the numerical results, the performances corrected by the FSI effects were proposed for the more reliable predictions.

Keywords

References

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