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dc.contributor.authorSun, Dakun
dc.contributor.authorGeng, Chunwang
dc.contributor.authorLi, Jia
dc.contributor.authorWang, Yuqing
dc.contributor.authorDong, Xu
dc.contributor.authorSun, Xiaofeng
dc.date.accessioned2026-08-23T08:19:16Z
dc.date.available2026-08-23T08:19:16Z
dc.date.copyright2026/03/01
dc.date.issued2026
dc.identifier.issn0889-504X
dc.identifier.otherturbo-25-1068.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4316382
dc.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.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleLocalized Disturbance Evolution Under Circumferential Distortion: A Perspective on the Critical Angle
dc.typeJournal Paper
dc.journal.volume148
dc.journal.issue3
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4069799
dc.journal.fristpage74
dc.journal.lastpage82
dc.page9
dc.treeJournal of Turbomachinery:;2026:;volume( 148 ):;issue:003
dc.contenttypeFulltext


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