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    Localized Disturbance Evolution Under Circumferential Distortion: A Perspective on the Critical Angle

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:003::page 74
    Author:
    Sun, Dakun
    ,
    Geng, Chunwang
    ,
    Li, Jia
    ,
    Wang, Yuqing
    ,
    Dong, Xu
    ,
    Sun, Xiaofeng
    DOI: 10.1115/1.4069799
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. This article aims to explain the formation mechanism and variation patterns of critical distortion angles through disturbance evolution on a low-speed fan. Based on time-domain analysis and wavelet transform, the pattern of the circumferential pre-stall disturbance evolution is revealed. An identical irreversible zone is observed by first-order spatial modal analysis within one revolution prior to stall, regardless of distortion angles. The foam metal casing treatment (FMCT) is used to generate modal and spike stall precursors separately in the same fan by adjusting the axial location. It is found that the critical distortion angle exists with “spike” but vanishes with “modal.” Averaged wavelet spectra of pre-stall disturbance under different distortions prove that disturbance evolution rates depend on local loading, not distortion area. At last, a simple qualitative model on the critical distortion angle is proposed, establishing a direct correlation between the development of short length-scale disturbance and stability limits.
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      Localized Disturbance Evolution Under Circumferential Distortion: A Perspective on the Critical Angle

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4316382
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    • Journal of Turbomachinery

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    contributor authorSun, Dakun
    contributor authorGeng, Chunwang
    contributor authorLi, Jia
    contributor authorWang, Yuqing
    contributor authorDong, Xu
    contributor authorSun, Xiaofeng
    date accessioned2026-08-23T08:19:16Z
    date available2026-08-23T08:19:16Z
    date copyright2026/03/01
    date issued2026
    identifier issn0889-504X
    identifier otherturbo-25-1068.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316382
    description abstractAbstract. This article aims to explain the formation mechanism and variation patterns of critical distortion angles through disturbance evolution on a low-speed fan. Based on time-domain analysis and wavelet transform, the pattern of the circumferential pre-stall disturbance evolution is revealed. An identical irreversible zone is observed by first-order spatial modal analysis within one revolution prior to stall, regardless of distortion angles. The foam metal casing treatment (FMCT) is used to generate modal and spike stall precursors separately in the same fan by adjusting the axial location. It is found that the critical distortion angle exists with “spike” but vanishes with “modal.” Averaged wavelet spectra of pre-stall disturbance under different distortions prove that disturbance evolution rates depend on local loading, not distortion area. At last, a simple qualitative model on the critical distortion angle is proposed, establishing a direct correlation between the development of short length-scale disturbance and stability limits.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLocalized Disturbance Evolution Under Circumferential Distortion: A Perspective on the Critical Angle
    typeJournal Paper
    journal volume148
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4069799
    journal fristpage74
    journal lastpage82
    page9
    treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:003
    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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