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    Stability Enhancement With Controllable Speed Casing for Transonic Compressor Rotor in Different Speed Conditions

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:005
    Author:
    Zhao, Jiayi
    ,
    Wu, Wanyang
    ,
    Zhong, Jingjun
    DOI: 10.1115/1.4070463
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. 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.
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      Stability Enhancement With Controllable Speed Casing for Transonic Compressor Rotor in Different Speed Conditions

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4316826
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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