Crossflow analogy를 이용한 미사일 동체의 공력 특성 예측A prediction of aerodynamic characteristics for missile body using crossflow analogy
- Advisors
- 박승오researcher; Park, Seung-Oresearcher
- Description
- 한국과학기술원 : 항공우주공학과,
- Publisher
- 한국과학기술원
- Issue Date
- 1999
- Identifier
- 150501/325007 / 000973518
- Language
- kor
- Description
학위논문(석사) - 한국과학기술원 : 항공우주공학과, 1999.2, [ vi, 38 p. ]
- Keywords
비례 계수; Slender Body 이론; 횡단면흐름; 항력 계수; Drag coefficient; Proportionality factor; Slender body theory; Crossflow
- Appears in Collection
- AE-Theses_Master(석사논문)
- Files in This Item
- There are no files associated with this item.
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