큰 깃배치각을 갖는 천음속 압축기 정익-동익 段유동에 관한 복합격자의 해Composite-Grid Solution to the Transonic Compressor Stator-Rotor Stage Flow at High Stagger Angle
- Publisher
- 한국항공우주학회
- Issue Date
- 1994-04
- Language
- English
- Citation
한국항공우주학회지, v.22, no.2, pp.36 - 45
- ISSN
- 1225-1348
- Appears in Collection
- AE-Journal Papers(저널논문)
- Files in This Item
- There are no files associated with this item.
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.