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contributor authorZhao, Jiayi
contributor authorWu, Wanyang
contributor authorZhong, Jingjun
date accessioned2026-08-23T08:37:37Z
date available2026-08-23T08:37:37Z
date copyright2026/05/01
date issued2026
identifier issn0889-504X
identifier otherturbo-25-1073.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316826
description abstractAbstract. Controllable speed casing (CSC) represents an innovative approach to casing treatment designed to enhance the adaptability of casing treatment to the variable operating conditions of compressors. This study investigates the stability enhancement mechanism and effects of CSC at different rotor speed conditions in a transonic compressor. The results indicate that CSC can improve flow stability by reducing the intensity of the shock/tip leakage vortex interaction to varying degrees when the rotor operates at 80–110% design speed. Furthermore, the stability enhancement effect increases with the rotating speed of the CSC. However, when the rotor speed decreases to 60% design speed, causing the tip flow field to transition to subsonic flow, the rotation of the CSC aggravates the backflow within the tip leakage flow, resulting in the loss of efficacy of stability enhancement.
publisherThe American Society of Mechanical Engineers (ASME)
titleStability Enhancement With Controllable Speed Casing for Transonic Compressor Rotor in Different Speed Conditions
typeJournal Paper
journal volume148
journal issue5
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4070463
treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:005
contenttypeFulltext


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