An investigation on tapered wings with leading edge tubercles
An experimental study was conducted to examine the flow around swept tapered wings with leading edge protuberances. Particle Imaging Velocimetry, a non-intrusive flow visualisation technique was conducted in a water tunnel. 2 wings with SD7032 airfoil profile and a mean aerodynamic chord of 82.15mm,...
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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2017
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| 在線閱讀: | http://hdl.handle.net/10356/72387 |
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| 機構: | Nanyang Technological University |
| 語言: | English |