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...

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Bibliographic Details
Published in:International journal of numerical methods for heat & fluid flow Vol. 33, № 6. P. 2278-2294
Other Authors: Yazdani, Shima, Salimipour, Erfan, Salimipour, Ayoob, Sheremet, Mikhail A., Ghalambaz, Mohammad
Format: Article
Language:English
Subjects:
Online Access:http://vital.lib.tsu.ru/vital/access/manager/Repository/koha:001133664
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245 1 0 |a Effects of coflow-jet active flow control on airfoil stall  |c S. Yazdani, E. Salimipour, A. Salimipour [et al.] 
336 |a Текст 
337 |a электронный 
520 3 |a 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 model are used to study the effects of coflow-jet (CFJ) on the dynamic and static stall phenomena. CFJ implementation is conducted with several momentum coefficients to investigate their turnover. Furthermore, the current work intends to analyze the CFJ performance by varying the Reynolds number and jet momentum coefficient and comparing all states to the baseline airfoil, which has not been studied in prior research investigations. Findings - It is observed that at the momentum coefficient (Cµ) of 0.06, the lift coefficients at low attack angles (up to a = 15) dramatically increase. Furthermore, the dynamic stall at the given Reynolds number and with the lowered frequency of 0.15 is explored. In the instance of Cµ = 0.07, the lift coefficient curve does not show a noticeable stall feature compared to Cµ = 0.05, suggesting that a more powerful stronger jet can entirely control the dynamic stall. Originality/value - Furthermore, the current work intends to analyze the CFJ performance by varying the jet momentum coefficient and comparing all states to the baseline airfoil, which has not been studied in prior research investigations. 
653 |a коэффициент импульса струи 
653 |a профили крыла 
653 |a Рейнольдса число 
653 |a динамическое сваливание 
653 |a коэффициент подъемной силы 
653 |a активное управление потоком 
655 4 |a статьи в журналах 
700 1 |a Yazdani, Shima 
700 1 |a Salimipour, Erfan 
700 1 |a Salimipour, Ayoob 
700 1 |a Sheremet, Mikhail A. 
700 1 |a Ghalambaz, Mohammad 
773 0 |t International journal of numerical methods for heat & fluid flow  |d 2023  |g Vol. 33, № 6. P. 2278-2294  |x 0961-5539 
852 4 |a RU-ToGU 
856 4 |u http://vital.lib.tsu.ru/vital/access/manager/Repository/koha:001133664 
908 |a статья 
999 |c 1133664  |d 1133664