Experimental Investigation on the Effects of Unsteady Excitation Frequency of Casing Treatment on Transonic Compressor PerformanceSource: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 002::page 21014DOI: 10.1115/1.4000581Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The importance of the unsteady effects between the casing treatment and rotor is still not clear. Experiments are conducted in a transonic compressor with arc skewed slot casing treatment configurations. The experimental results indicate that the unsteady excitation frequency due to the slot number of casing treatment is one of the most important factors influencing compressor performance. Also, compressor performance can be overall enhanced through optimizing this unsteady excitation frequency. For the transonic compressor herein, peak efficiency, stall margin, and maximum flow mass can be improved by 0.17%, 19.86%, and 0.81%, respectively, at near design rotating speed, which can reach up to 1.13%, 57.84%, and 1.57%, respectively, at part design speed.
keyword(s): Flow (Dynamics) , Compressors , Design AND Rotors ,
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contributor author | Wei Tuo | |
contributor author | Yajun Lu | |
contributor author | Wei Yuan | |
contributor author | Sheng Zhou | |
contributor author | Qiushi Li | |
date accessioned | 2017-05-09T00:47:27Z | |
date available | 2017-05-09T00:47:27Z | |
date copyright | April, 2011 | |
date issued | 2011 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28770#021014_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/147832 | |
description abstract | The importance of the unsteady effects between the casing treatment and rotor is still not clear. Experiments are conducted in a transonic compressor with arc skewed slot casing treatment configurations. The experimental results indicate that the unsteady excitation frequency due to the slot number of casing treatment is one of the most important factors influencing compressor performance. Also, compressor performance can be overall enhanced through optimizing this unsteady excitation frequency. For the transonic compressor herein, peak efficiency, stall margin, and maximum flow mass can be improved by 0.17%, 19.86%, and 0.81%, respectively, at near design rotating speed, which can reach up to 1.13%, 57.84%, and 1.57%, respectively, at part design speed. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Experimental Investigation on the Effects of Unsteady Excitation Frequency of Casing Treatment on Transonic Compressor Performance | |
type | Journal Paper | |
journal volume | 133 | |
journal issue | 2 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4000581 | |
journal fristpage | 21014 | |
identifier eissn | 1528-8900 | |
keywords | Flow (Dynamics) | |
keywords | Compressors | |
keywords | Design AND Rotors | |
tree | Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 002 | |
contenttype | Fulltext |