The KSFM Journal of Fluid Machinery (한국유체기계학회 논문집)

Korean Society for Fluid machinery (한국유체기계학회)
권호 표지
DOI QR코드

DOI QR Code

Numerical Flow Analysis of a Supersonic Impulse Turbine with Nozzles and Rotor Blades

노즐과 로터가 장착된 초음속 충동형 터빈의 전산유동해석

  • 박편구 (한국항공우주연구원 터보펌프팀) ;
  • 이은석 (한국항공우주연구원 엔진팀) ;
  • 정은환 (한국항공우주연구원 터보펌프팀) ;
  • 김진한 (한국항공우주연구원 터보펌프팀)
  • Published : 2007.02.01
Download PDF
⟨ Previous Next ⟩

Abstract

Four design candidates for a partial admission turbine have been chosen from a preliminary design process. Their performance were estimated through the 3-D numerical analyses using a frozen rotor method. In order to select the optimum design, each flow analysis result was compared with others. Flow characteristics in the passages and some types of losses induced by shocks and wakes were found from calculation results. Based on these calculations, a new rotor blade was redesigned and compared with previous one through flow analysis.

Keywords

References

  1. 김진한, 홍순삼, 최창호, 전성민, 정은환, 2005, '30톤급 액체로켓엔진용 터보펌프 개발현황,' 한국추진공학회 2005년도 추계학술대회 논문집, pp. 375-383
  2. Griffin, L. W. and Dorney, D. J., 2000, 'Simulation of the Unsteady Flow Through the Fastrac Supersonic Turbine,' Journal of Turbomachinery, Vol. 122, pp. 225-233 https://doi.org/10.1115/1.555453
  3. Giles, M. B., 1990, 'Stator/Rotor Interaction in a Transonic Turbine,' Journal of Propulsion, pp. 621-627
  4. Chima, R. V., 1998, 'Calculation of Multistage Turbomachinery Using Steady Characteristic Boundary Condition,' AIAA 98-0968
  5. FINETM/Turbo User Manual Version 6,1-a, pp. 5-3-5-22
  6. 박편구, 정은환, 김진한, 2005, '유로형상변화에 따른 터빈성능 변화의 수치적 해석,' 2005년도 유체기계 연구개발 발표회, pp. 481-486
  7. Hodson, H. P., 1998, 'Blade Row Interference Effects in Axial Turbomachinery Stages,' Von Karman Institute for Fluid Dynamics, Lecture Series 1998-02
  8. 박편구, 이은석, 정은환, 김진한, 2004, '1.4MW급 부분 흡입형 터빈의 유동해석,' 2004년 한국군사과학기술학회 종합학술대회논문집, Vol. II, pp. 590-593