Oscillating Flap Excitation Control of a Dynamic Stall Seperation Flow Over a Wing
碩士 === 國立成功大學 === 航空太空工程學系 === 83 === The active control of separated and unsteady flow over NACA 633-018 cross section airfoil at high angle of attack is studied experimentally by means of a leading-edged periodic oscillating flap located...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
1995
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| Online Access: | http://ndltd.ncl.edu.tw/handle/06526828570004776672 |