Investigation of low aspect-ratio effect on thin-plate wing at low Reynolds numbers
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 93 === The thesis experimentally studies the aerodynamic performances and the corresponding flow structures on thin-plate wings with aspect ratios between 1.0 and 2.0 and Reynolds numbers between 5x104~1x105 in a low speed wing tunnel. The measurements of the win...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2005
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| Online Access: | http://ndltd.ncl.edu.tw/handle/58605015621596743458 |