Streamwise and spanwise plasma actuators for flow-induced cavity noise control
Huang, Xun and Zhang, Xin (2008) Streamwise and spanwise plasma actuators for flow-induced cavity noise control. Physics of Fluids, 20, (3), 037101-[10pp]. (doi:10.1063/1.2890448).
- Publishers print
Plasma actuators operating in atmospheric air can induce a body force through collisions between electrically charged particles and neutral air molecules by an externally applied electric field. The fast response and the simple structure make the plasma actuator a promising option in aerospace applications. In this work, experiments were performed with several alternative current excited plasma (streamwise and spanwise) actuators to control flow-induced noise from a cavity. It was found that the streamwise actuator induced three-dimensional variations in the shear layer. The spanwise actuator, however, has little influence on the global flow field. As a result, the streamwise actuator is more effective than the spanwise actuator in cavity noise attenuation.
|Subjects:||T Technology > TL Motor vehicles. Aeronautics. Astronautics
Q Science > QC Physics
|Divisions:||University Structure - Pre August 2011 > School of Engineering Sciences > Aerodynamics & Flight Mechanics
|Date Deposited:||17 Mar 2008|
|Last Modified:||25 Apr 2013 16:16|
|Contributors:||Huang, Xun (Author)
Zhang, Xin (Author)
|Date:||12 March 2008|
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
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