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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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