Delaying leading edge vortex detachment by plasma flow control at topologically critical locations

نویسندگان

چکیده

Leading edge vortices on flapping wings induce high transient lift during their growth phase and increase maneuverability at low flight speeds. A hypothesis is developed experimentally validated that the vortex a pitching plunging airfoil can be prolonged with dielectric barrier discharge plasma actuators. This demonstrated for various airfoils different motion dynamics kinematics.

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ژورنال

عنوان ژورنال: Physical review fluids

سال: 2021

ISSN: ['2469-9918', '2469-990X']

DOI: https://doi.org/10.1103/physrevfluids.6.023101