Bluff Body Noise and Flow Control with Atmospheric Plasma Actuators

Plasma actuators operating in atmospheric air were employed to modify aerodynamic flow over a bluff body. The model consisted of a cylinder and a torque link that was installed on the lee side of the cylinder. The objective was to reduce the broadband noise that is mainly generated by the impingement of the cylinder wake on the torque link. The plasma actuators were configured to produce dielectric barrier discharges, through which the flow separation from the cylinder was enhanced by the externally imposed body force. As a result the flow-structure interaction between the wake and the torque link was reduced, leading to the attenuation of broadband noise. The noise and flow control performance with the plasma actuators were studied in an anechoic chamber facility as well as in a wind tunnel facility by examining sound pressure and mean flow field respectively. With the current plasma actuators, it was found that there was 1 dB reduction in overall sound pressure level at a free stream speed of 30 m/s, and the wake speed impinging on the torque link was reduced. A possible solution to improve the broadband noise attenuation performance is discussed at the end of this paper.

[1]  Mohamed Gad-el-Hak,et al.  Flow Control: Passive, Active, and Reactive Flow Management , 2000 .

[2]  Xun Huang,et al.  Streamwise and spanwise plasma actuators for flow-induced cavity noise control , 2008 .

[3]  D. K. McLaughlin,et al.  Recent Aeroacoustics Research in the United States , 2000 .

[4]  J. Roth,et al.  Aerodynamic flow acceleration using paraelectric and peristaltic electrohydrodynamic effects of a One Atmosphere Uniform Glow Discharge Plasma , 2003 .

[5]  Xun Huang,et al.  Atmospheric Plasma Actuators for Aeroacoustic Applications , 2007, IEEE Transactions on Plasma Science.

[6]  E. Moreau,et al.  Optimization of a dielectric barrier discharge actuator by stationary and non-stationary measurements of the induced flow velocity: application to airflow control , 2007 .

[7]  J. R. Roth Electrohydrodynamically induced airflow in a one atmosphere uniform glow discharge surface plasma , 1998, 25th Anniversary, IEEE Conference Record - Abstracts. 1998 IEEE International Conference on Plasma Science (Cat. No.98CH36221).

[8]  Thomas Corke,et al.  Plasma Actuators for Landing Gear Noise Reduction , 2005 .

[9]  Eric Moreau,et al.  Airflow control by non-thermal plasma actuators , 2007 .

[10]  Xin Zhang,et al.  The attenuation of cavity tones using plasma actuators , 2005 .

[11]  Xun Huang,et al.  Variable structure model for flow-induced tonal noise control with plasma actuators , 2007 .

[12]  Xin Zhang,et al.  Attenuation of Low-Speed Flow-Induced Cavity Tones Using Plasma Actuators , 2007 .

[13]  J. Roth,et al.  Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma , 2000 .

[14]  Wookyung Kim,et al.  Aerodynamic modification of flow over bluff objects by plasma actuation , 2006 .