3-D Near-Wake Flow Investigation behind a Low-Aspect-Ratio Wing at a Low Reynolds number
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 97 === This study investigates the near-wake flow structures behind a flat-plate wing at different angles of attack. The flat-plate wing model with AR = 1 is operated at freestream velocity of 10m/s and the corresponding Reynolds number based on the chord length is...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2009
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| Online Access: | http://ndltd.ncl.edu.tw/handle/02366428486084080119 |