Experimental studies on the development of finite-wing wake
碩士 === 國立成功大學 === 航空太空工程學系 === 90 === The characteristics of the wake development of a finite wing under 3 different angles of attack were studied through experimental means. X-type hotwire anemometer was utilized to measure both the velocity of x and y direction of the three-dimensional...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2002
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| Online Access: | http://ndltd.ncl.edu.tw/handle/70702648529893404894 |