NUMERICAL STUDY ON THE TURBOPUMP INDUCER

터보펌프 인듀서에 대한 수치해석적 연구

  • 노준구 (한국항공우주연구원 터보펌프그룹) ;
  • 최창호 (한국항공우주연구원 터보펌프그룹) ;
  • 홍순삼 (한국항공우주연구원 터보펌프그룹) ;
  • 김진한 (한국항공우주연구원 터보펌프그룹)
  • Published : 2005.10.01

Abstract

The present study focuses on the flow analysis of a turbopump inducer by performing both numerical and experimental methods. The head rise, efficiency and detailed flow fields such as outlet flow angles, pressure and velocity vectors are measured and compared with the computational data. Generally a good agreement is obtained between numerical and experimental results. However, some discrepancies are observed due to complex flow structures inside the inducer. Future calculations with an advanced turbulence model and a dense computational grid needs to be performed to obtain accurate numerical solution for the detailed flow fields.

Keywords