Numerical Study of Airfoil Flow at High Angle of Attack
碩士 === 國立成功大學 === 航空太空工程學系 === 88 === The study applies a Navier-Stokes solver to probe the characteristics of flow of aerodynamics of a NACA0012 airfoil. The solver uses a third-order upwind finite-volume method and modified Osher-Chakravarthy method. The method also uses an implicit res...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/41604183620208476097 |