The Effect of Aspect Ratio on the Performance of Airfoil with Protuberances on Leading Edges
碩士 === 國立成功大學 === 系統及船舶機電工程學系碩博士班 === 98 === This study investigated the effect of aspect ratio and shape of protuberances on the performance of airfoil with protuberances on leading edge. NACA0012 foil is used for modifying the leading edge with three different forms and three aspect ratios (1, 2,...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2010
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| Online Access: | http://ndltd.ncl.edu.tw/handle/58893975071017401393 |