유체 구조 연계 해석기법을 적용한 터보블로워 공력성능 해석에 관한 수치적 연구

Numericla Study on the Aerodynamic Performances of the Turbo Blower Using Fluid-Structure Interaction Method
  • 정희택
  • 박태규
  • 김형범
  • 박준영

초록

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.

키워드

Fluid-Structure InteractionTurbo BlowerTip ClearanceAerodynamic Performance유체-구조 연계 해석터보블로워팁 간극공력성능
제목
유체 구조 연계 해석기법을 적용한 터보블로워 공력성능 해석에 관한 수치적 연구
제목 (타언어)
Numericla Study on the Aerodynamic Performances of the Turbo Blower Using Fluid-Structure Interaction Method
저자
정희택박태규김형범박준영
발행일
2011
저널명
동력시스템공학회지
15
6
페이지
35 ~ 40