오일러 방정식을 이용한 비행체 날개의 천음속 플러터 해석 = Transonic flutter analysis for airfoils and wings using euler equations

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Advisors
이인researcherLee, Inresearcher
Description
한국과학기술원 : 항공우주공학과,
Publisher
한국과학기술원
Issue Date
1996
Identifier
105507/325007 / 000885260
Language
kor
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학과, 1996.2, [ x, 135 p. ]

Keywords

과도충격법; 표면보간법; 연계적분법; U-g; 플랩단면모델; 유한요소법; 일반력; 정상 및 비정상공기력; 오일러방정식; 유한체적법; 천음속 플러터; 공탄성; 등방성 및 복합재 날개; Isotropic and Composite Wing; Flap Typical Section; U-G; Coupled Time-Integration Method; Surface Spline Method; Transient Pulse Method; Aeroelasticiy; Transonic Flutter; CFD; Euler Equation; Steady and Unsteady Aerodynamics; Generalized Aerodynamic Forces; FEM

URI
http://hdl.handle.net/10203/26217
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=105507&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
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