This paper proposes a new technique to reduce the noise generated by rotor-stator interaction (tonal noise) in fans and compressors. The method involves the use of single dielectric barrier discharge (plasma) actuators near the blade trailing edge to reduce blade wakes. Plasma actuators are a new and simple type of active flow control device consisting of two parallel and offset electrodes separated by a layer of dielectric material. The application of a high ac voltage at high frequency to the electrodes generates a body force on the flow in the vicinity of the electrodes to inject momentum without mass addition. A preliminary assessment of the proposed concept is performed with a computational study on modern low-speed compressor rotor geometry. A plasma actuator model is implemented in an established turbomachinery CFD code. Simulations are carried out to evaluate the effect of the actuator strength, location, and actuation method (continuous versus pulsed) on the rotor wake. Results show that plasma actuators operated in continuous mode near the trailing edge can significantly influence the wake of the rotor with relatively little power consumption. The effectiveness of the actuation is proportional to actuator strength (induced body force). The exact position of the actuator in the trailing edge region has little effect on the effectiveness of the actuation. The results from simulations with pulsed actuation show very low time-averaged influence on the wake and are not fully conclusive, due possibly to the frequencies simulated and the limitations of the RANS CFD tool.
Skip Nav Destination
Article navigation
January 2011
Research Papers
Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction
Sébastien Lemire,
Sébastien Lemire
Department of Mechanical Engineering,
École Polytechnique de Montréal
, Montreal, QC H3T 1J4, Canada
Search for other works by this author on:
Huu Duc Vo
Huu Duc Vo
Department of Mechanical Engineering,
École Polytechnique de Montréal
, Montreal, QC H3T 1J4, Canada
Search for other works by this author on:
Sébastien Lemire
Department of Mechanical Engineering,
École Polytechnique de Montréal
, Montreal, QC H3T 1J4, Canada
Huu Duc Vo
Department of Mechanical Engineering,
École Polytechnique de Montréal
, Montreal, QC H3T 1J4, CanadaJ. Turbomach. Jan 2011, 133(1): 011017 (11 pages)
Published Online: September 22, 2010
Article history
Received:
June 20, 2009
Revised:
July 18, 2009
Online:
September 22, 2010
Published:
September 22, 2010
Citation
Lemire, S., and Vo, H. D. (September 22, 2010). "Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction." ASME. J. Turbomach. January 2011; 133(1): 011017. https://doi.org/10.1115/1.4000540
Download citation file:
Get Email Alerts
Guideline for Large-Scale Analysis of Centrifugal Blower Using Wall-Resolved Large Eddy Simulation
J. Turbomach (February 2025)
Related Articles
A Correlation-Based Transition Model Using Local Variables—Part II:
Test Cases and Industrial Applications
J. Turbomach (January,0001)
The Effect of Wake Induced Structures on Compressor Boundary-Layers
J. Turbomach (October,2007)
An Investigation of Wake-Shock Interactions in a Transonic Compressor With Digital Particle Image Velocimetry and Time-Accurate Computational Fluid Dynamics
J. Turbomach (October,2006)
Plasma-Based Flow-Control Strategies for Transitional Highly Loaded Low-Pressure Turbines
J. Fluids Eng (April,2008)
Related Proceedings Papers
Related Chapters
CFD Analysis of Propeller Tip Vortex Cavitation in Ship Wake Fields
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Computational Modeling of Dynamic Planing Forces
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Aerodynamic Performance Analysis
Axial-Flow Compressors