Effects of coflow-jet active flow control on airfoil stall
Purpose - Active flow control on the NACA 0024 airfoil defined as suction-injection jet at the chord-based Reynolds number of 1.5 × 1e + 5 is studied. Design/methodology/approach - The three-dimensional incompressible unsteady Reynolds-averaged Navier–Stokes equations with the SST k-ω turbulence mod...
| Опубликовано в: : | International journal of numerical methods for heat & fluid flow Vol. 33, № 6. P. 2278-2294 |
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| Другие авторы: | , , , , |
| Формат: | Статья в журнале |
| Язык: | English |
| Предметы: | |
| Online-ссылка: | http://vital.lib.tsu.ru/vital/access/manager/Repository/koha:001133664 |