Investigation on Flow Structure for Low-Aspect Ratio Wing at Critical Reynolds Numbers
碩士 === 國立成功大學 === 航空太空工程學系 === 103 === For developing unmanned aerial vehicles (UAVs), micro air vehicles (MAV) and small-scale wind turbine blades, understanding the relationship between the flow structure and aerodynamic performance of NACA series wings is required. Most of the previous studies we...
| Main Authors: | , |
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| Format: | Others |
| Language: | en_US |
| Published: |
2015
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| Online Access: | http://ndltd.ncl.edu.tw/handle/20170999235867738248 |