Active flow control for drag reduction of a plunging airfoil under deep dynamic stall

Active flow control for drag reduction of a plunging airfoil under deep dynamic stall

Brener L. O. Ramos, William R. Wolf, Yeh Chi-An, Kunihiko Taira

ARTIGO

Inglês

Agradecimentos: CENAPAD-SP [551]; US Air Force Office of Scientific ResearchUnited States Department of DefenseAir Force Office of Scientific Research (AFOSR) [FA9550-18-1-0040]

High-fidelity simulations are performed to study active flow control techniques for alleviating deep dynamic stall of an SD7003 airfoil in plunging motion. The flow Reynolds number is Re = 60 000 and the freestream Mach number is M = 0.1. Numerical simulations are performed with a...

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Fechado

Active flow control for drag reduction of a plunging airfoil under deep dynamic stall

Brener L. O. Ramos, William R. Wolf, Yeh Chi-An, Kunihiko Taira


										

Active flow control for drag reduction of a plunging airfoil under deep dynamic stall

Brener L. O. Ramos, William R. Wolf, Yeh Chi-An, Kunihiko Taira

    Fontes

    Physical review fluids

    Vol. 4, no. 7 (July, 2019), n. art. 74603