오일러 방정식을 이용한 비행체 날개의 천음속 플러터 해석Transonic flutter analysis for airfoils and wings using euler equations
- Advisors
- 이인researcher; Lee, 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
- Appears in Collection
- AE-Theses_Ph.D.(박사논문)
- Files in This Item
- There are no files associated with this item.
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