| contributor author | Sébastien Lemire | |
| contributor author | Huu Duc Vo | |
| date accessioned | 2017-05-09T00:47:36Z | |
| date available | 2017-05-09T00:47:36Z | |
| date copyright | January, 2011 | |
| date issued | 2011 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28767#011017_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/147868 | |
| description abstract | 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. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction | |
| type | Journal Paper | |
| journal volume | 133 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4000540 | |
| journal fristpage | 11017 | |
| identifier eissn | 1528-8900 | |
| keywords | Force | |
| keywords | Flow (Dynamics) | |
| keywords | Compressors | |
| keywords | Plasmas (Ionized gases) | |
| keywords | Wakes | |
| keywords | Actuators | |
| keywords | Rotors | |
| keywords | Blades | |
| keywords | Momentum | |
| keywords | Engineering simulation | |
| keywords | Noise control | |
| keywords | Electrodes | |
| keywords | Computational fluid dynamics | |
| keywords | Noise (Sound) AND Stators | |
| tree | Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001 | |
| contenttype | Fulltext | |