Detailed Information
Cited 0 time in 
Cited 0 time in 
Cited 0 time in
Metadata Downloads
디퓨저 깃배치각의 변화에 따른 원심압축기의 공력성능 특성에 관한 수치 연구NUMERICAL INVESTIGATION OF THE EFFECT OF THE STAGGER ANGLE ON THE AERODYNAMIC PERFORMANCES IN THE VANED DIFFUSER OF A CENTRIFUGAL COMPRESSOR
- Other Titles
- NUMERICAL INVESTIGATION OF THE EFFECT OF THE STAGGER ANGLE ON THE AERODYNAMIC PERFORMANCES IN THE VANED DIFFUSER OF A CENTRIFUGAL COMPRESSOR
- Issue Date
- 2010
- Publisher
- 한국전산유체공학회
- Keywords
- 공력성능(Aerodynamic Performance); 깃 배치각(Stagger Angle); 원심압축기(Centrifugal Compressor); 디퓨저(Diffuser)
- Citation
- 한국전산유체공학회지, v.15, no.3, pp 60 - 65
- Pages
- 6
- Indexed
- KCI
- Journal Title
- 한국전산유체공학회지
- Volume
- 15
- Number
- 3
- Start Page
- 60
- End Page
- 65
- ISSN
- 1598-6071
- Abstract
- In the present study, the effects of the stagger angles on the aerodynamic performances in the vaned centrifugal compressor has been investigated by CFD methods. The diffuser vane angles were varied in the range of ±10 deg. from the initial-design points. The commercial Navier-Stokes solver, ANSYS-CFX were applied to solve the impeller-diffuser flowfields. Through the numerical results, the desirable setting angles were proposed to fit the best performance to the variation of the operating conditions.
- Files in This Item
- There are no files associated with this item.
- Appears in
Collections - 공과대학 > Department of Mechanical Engineering > Journal Articles
Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.