An experimental investigation on tapered wings with leading-edge protuberances
Particle Image Velocimetry (PIV) experiments were conducted in a water tunnel to study vortex interactions around tapered swept wings with leading edge tubercles. Two airfoil models based on the SD7032 airfoil profile were tested at Reynolds number 9100 and angles of attack (α) of -10°,10° and 25°,...
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| 格式: | Final Year Project |
| 語言: | English |
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Nanyang Technological University
2023
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| 在線閱讀: | https://hdl.handle.net/10356/168370 |
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| 機構: | Nanyang Technological University |
| 語言: | English |