Flow and Aerodynamic Performance of Back-Swept Wings
碩士 === 國立臺灣科技大學 === 機械工程系 === 94 === Effects of the back-swept angle, chord Renolds number, and root angle-of-attack on the surface flow and the aerodynamic performance of a finite back-swept wing are experimentally studied. The experiments are conducted in a wind tunnel. The cross-sectional profile...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2006
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| Online Access: | http://ndltd.ncl.edu.tw/handle/m9qv72 |