롤 운동을 고려한 발사체 곡면날개의 플러터 해석Flutter analysis of launch vehicle curved fin considering roll motion
- Advisors
- 이인researcher; Lee, Inresearcher
- Description
- 한국과학기술원 : 항공우주공학과,
- Publisher
- 한국과학기술원
- Issue Date
- 1998
- Identifier
- 133594/325007 / 000935174
- Language
- kor
- Description
학위논문(박사) - 한국과학기술원 : 항공우주공학과, 1998.2, [ x, 181 p. ]
- Keywords
Roll spin; Wrap-around fin(WAF); 오일러 방정식; 플러터; 공력탄성학; 롤 회전; 곡면 날개; Aeroelasticity; Delamination buckling; Post buckling analysis; Buckling; Composite laminated panel; Multiple delaminations; Euler equations; Flutter
- Appears in Collection
- AE-Theses_Ph.D.(박사논문)
- Files in This Item
- There are no files associated with this item.
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