Effect of dielectric barrier discharge plasma actuator on the dynamic moment behavior of pitching airfoil at low Reynolds number
The purpose of this paper is to investigate the feasibility of using dielectric barrier discharge
plasma actuation for the pitch stability control of a National Advisory Committee for …
plasma actuation for the pitch stability control of a National Advisory Committee for …
Unified mechanisms for separation control around airfoil using plasma actuator with burst actuation over Reynolds number range of 103–106
We conduct large-eddy simulations of separated airfoil flows with control by a dielectric-
barrier-discharge plasma actuator over a wide range of Reynolds numbers. The Reynolds …
barrier-discharge plasma actuator over a wide range of Reynolds numbers. The Reynolds …
Control of cavity flow with acoustic radiation by an intermittently driven plasma actuator
In a cavity flow with acoustic radiation, self-sustained oscillations are controlled by a
continuously or intermittently driven plasma actuator with elongated electrodes in the …
continuously or intermittently driven plasma actuator with elongated electrodes in the …
Flow control around NACA0015 airfoil using a dielectric barrier discharge plasma actuator over a wide range of the Reynolds number
In this study, an experimental investigation of separation control using a dielectric barrier
discharge plasma actuator was performed on an NACA0015 airfoil over a wide range of …
discharge plasma actuator was performed on an NACA0015 airfoil over a wide range of …
Post-stall flow control using a sawtooth plasma actuator in burst mode
Experimentally investigation is conducted on the control of post-stall airfoil aerodynamics
using a vortex-generator type plasma actuator (VG-PA), in burst mode (BM) at a Reynolds …
using a vortex-generator type plasma actuator (VG-PA), in burst mode (BM) at a Reynolds …
Suppression of deep cavity aeroacoustics at low Mach number by localized surface compliance
A unique concept of utilizing localized surface compliance is proposed to suppress deep
cavity aeroacoustics at a low Mach number. The core idea is to provide local absorption of …
cavity aeroacoustics at a low Mach number. The core idea is to provide local absorption of …
Superposition of AC-DBD plasma actuator outputs for three-dimensional disturbance production in shear flows
This investigation explores the utility of Alternating Current, Dielectric Barrier Discharge (AC-
DBD) plasma actuators for producing three-dimensional disturbances of a desired spanwise …
DBD) plasma actuators for producing three-dimensional disturbances of a desired spanwise …
Response of a turbulent separation bubble to zero-net-mass-flux jet perturbations
The response of a turbulent separation bubble (TSB) to zero-net-mass-flux actuation is
investigated via direct numerical simulations. Rectangular jets with their long axis oriented in …
investigated via direct numerical simulations. Rectangular jets with their long axis oriented in …
Mechanisms of morphing wall flow control by traveling waves over an airfoil
The main two mechanisms of morphing wall flow control are direct injection of momentum in
the streamwise direction and indirect momentum transfer via triggering instabilities …
the streamwise direction and indirect momentum transfer via triggering instabilities …
Effect of flow structure frequency on flow separation control using dielectric barrier discharge actuator
A better understanding of the mechanism of flow separation suppression by a dielectric
barrier discharge is essential for flow control. This paper investigates the mechanism of …
barrier discharge is essential for flow control. This paper investigates the mechanism of …