APPLICATION OF WEAKLY-IONIZED PLASMAS AS WING FLOW-CONTROL DEVICES

By Thomas C. Corke, E. Jumper, Martiqua L. Post, D. Orlov, Thomas McLaughlin. 2002

267 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Electrical and Electronic Engineering, Radiology, Nuclear Medicine and Imaging

View Paper: https://www.semanticscholar.org/paper/a325c7948706cfc349d37c5222f5afb855fa2c9e

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In Aerospace Engineering

In Electrical and Electronic Engineering

In Radiology, Nuclear Medicine and Imaging

Citations in the corpus

Scaling Effects of an Aerodynamic Plasma Actuator (2007, background): “Examples include boundarylayer control [12], lift augmentation on wings [13], separation control for low-pressure turbine blades [14], leading-edge separation control on wing sections [15], phased plasma arrays for unsteady flow control [16], and control of the dynamic stall vortex on oscillating ai”
Separation Control Using Plasma Actuators: Dynamic Stall Vortex Control on Oscillating Airfoil (2006, methodology): “These include lift augmentation on a wing section [22], low-pressure turbine blade separation control [23], airfoil leading-edge separation control [16,24], and plasma flaps and slats [25].”
Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications (2009, background): “5 [48, 7, 65], lift augmentation on a wing section [11, 13, 71, 84, 31, 30], low-pressure turbine blade separation control [36, 37, 38, 56, 107, 98, 97], turbine tip clearance flow control [68, 18, 113], bluff body flow control [111, 1, 17], turbulent boundary layer control [117, 39, 2, 88], unstead”
Active cancellation of artificially introduced Tollmien–Schlichting waves using plasma actuators (2008, background): “Many studies demonstrate the successful control and delay of flow separation on an inclined airfoil using plasma actuators (Corke and He 2004; Corke et al. 2002; Grundmann and Tropea 2005).”
Plasma Flaps and Slats: An Application of Weakly Ionized Plasma Actuators (2004, methodology): “[10] that examined the effect of from one to four plasma actuators located between x=c 0:72 and 0.”
Modeling of dielectric barrier discharge plasma actuators driven by repetitive nanosecond pulses (2007, background): “Asymmetric dielectric barrier discharge (DBD) plasma actuators are known to be effective in aerodynamic control [1-16].”
Experimental transition delay using glow-discharge plasma actuators (2007, background): “Numerous publications have shown the successful control and delay of flow separation on an airfoil using plasma actuators operated in pulsed mode (Corke and He 2004; Corke et al. 2002; Grundmann and Tropea 2005).”