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doi.org/10.1016/j.ast.2020.106251
Post-stall flow control using a sawtooth plasma actuator in burst mode
Longjun Wang
14
,
C. W. Wong
15
,
...,
Yu Zhou
37
View all 4 authors
Aerospace Science and Technology
5.80
Volume: 107, Pages: 106251 - 106251
Published
: Oct 2, 2020
23
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Paper Fields
Physics
Reynolds number
Mechanics
Airfoil
Aerodynamics
Vortex
Engineering
Vortex generator
Sawtooth wave
Lift coefficient
Plasma actuator
Turbulence
NACA airfoil
Freestream
Angle of attack
Stall (fluid mechanics)
Quantum mechanics
Plasma
Telecommunications
Dielectric barrier discharge
Paper Details
Title
Post-stall flow control using a sawtooth plasma actuator in burst mode
DOI
doi.org/10.1016/j.ast.2020.106251
Published Date
Oct 2, 2020
Journal
Aerospace Science and Technology
Volume
107
Pages
106251 - 106251
Notes
History
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