롤 운동을 고려한 발사체 곡면날개의 플러터 해석 = Flutter analysis of launch vehicle curved fin considering roll motion

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Advisors
이인researcherLee, 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

URI
http://hdl.handle.net/10203/26237
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=133594&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
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