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contributor authorSébastien Lemire
contributor authorHuu Duc Vo
date accessioned2017-05-09T00:47:36Z
date available2017-05-09T00:47:36Z
date copyrightJanuary, 2011
date issued2011
identifier issn0889-504X
identifier otherJOTUEI-28767#011017_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/147868
description abstractThis 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleReduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction
typeJournal Paper
journal volume133
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4000540
journal fristpage11017
identifier eissn1528-8900
keywordsForce
keywordsFlow (Dynamics)
keywordsCompressors
keywordsPlasmas (Ionized gases)
keywordsWakes
keywordsActuators
keywordsRotors
keywordsBlades
keywordsMomentum
keywordsEngineering simulation
keywordsNoise control
keywordsElectrodes
keywordsComputational fluid dynamics
keywordsNoise (Sound) AND Stators
treeJournal of Turbomachinery:;2011:;volume( 133 ):;issue: 001
contenttypeFulltext


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