Investigation on Aerodynamics and Flow Properties of a Low-Aspect-Ratio Thin-Plate Wing at Low Reynolds Number
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 96 === This thesis studies the flow structures of wing tip vortex on thin-plate wing at different angles of attack. The thin-plate wing model with AR = 1 was operated at free-stream velocity of 13m/s, corresponding to chord-based Reynolds number of 8×10^4. The wing...
| Main Authors: | , |
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| Format: | Others |
| Language: | en_US |
| Published: |
2008
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| Online Access: | http://ndltd.ncl.edu.tw/handle/24481371667645704010 |