Numerical Investigation on Flow Separation Control of Low Reynolds Number Sinusoidal Aerofoils
The paper presents a computational analysis of the characteristics of a NACA 634-021 aerofoil incorporated with sinusoidal leading-edge protuberances at Re = 14,000. The protuberances are characterized by an amplitude and wavelength of 12% and 50% of the aerofoil chord length respectively. An unstea...
| Үндсэн зохиолчид: | , , |
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| Бусад зохиолчид: | |
| Формат: | Conference Paper |
| Хэл сонгох: | English |
| Хэвлэсэн: |
2017
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| Нөхцлүүд: | |
| Онлайн хандалт: | https://hdl.handle.net/10356/83344 http://hdl.handle.net/10220/42539 |