Loss Model과 combined Blade Element 방법을 이용한 팬덕트 테일로터의 성능 해석 및 저소음화

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Publisher
한국항공우주학회
Issue Date
2004-11
Language
KOR
Citation

2004 항공우주학회 추계학술대회, pp.764 - 767

URI
http://hdl.handle.net/10203/145619
Appears in Collection
AE-Conference Papers(학술회의논문)
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