선형 안정성 이론을 이용한 압축성 축대칭 원뿔 경계층 천이지점 예측Transition Prediction of Compressible Axi-symmetric Cone Boundary Layer based on Linear Stability Theory
- Publisher
- 한국항공우주학회
- Issue Date
- 2007-11-15
- Language
- KOR
- Citation
한국항공우주학회 학술발표회, pp.33 - 36
- Appears in Collection
- AE-Conference Papers(학술회의논문)
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