Control of crossflow instability over a swept wing using dielectric-barrier-discharge plasma actuators
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DOI: 10.1016/j.ijheatfluidflow.2018.07.012
Abstract: Abstract This paper investigates the potential use of dielectric-barrier-discharge (DBD) plasma actuators to control the crossflow instability of the boundary layer on a 45° swept NLF-0415 airfoil at − 4 ∘ angle of attack.The disturbance… read more here.
Keywords: crossflow instability; dielectric barrier; barrier discharge; plasma actuators ... See more keywords