Surface Flow and Vortex Shedding of an Impulsively Started Wing
碩士 === 國立臺灣科技大學 === 機械工程系 === 87 === The particle tracking flow visualization method (PTFV) and particle imagine velocimetry (PIV) were used to obtain a clear picture of the vortex evolution process on suction surface of an impulsively started NACA 0012 wing. The formation and evolution p...
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
1999
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| Online Access: | http://ndltd.ncl.edu.tw/handle/18912332677841842695 |