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

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Publisher
한국항공우주학회
Issue Date
1994-04
Language
English
Citation

한국항공우주학회지, v.22, no.2, pp.36 - 45

ISSN
1225-1348
URI
http://hdl.handle.net/10203/59048
Appears in Collection
AE-Journal Papers(저널논문)
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