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contributor authorV. H. Garnier
contributor authorA. H. Epstein
contributor authorE. M. Greitzer
date accessioned2017-05-08T23:37:00Z
date available2017-05-08T23:37:00Z
date copyrightApril, 1991
date issued1991
identifier issn0889-504X
identifier otherJOTUEI-28609#290_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109434
description abstractStall inception has been studied in two low-speed compressors (a single-stage and a three-stage) and in a high-speed three-stage compressor, using temporally and spatially resolved measurements. In all three machines, rotating stall was preceded by a period in which small-amplitude waves were observed traveling around the circumference of the machine at a speed slightly less than the fully developed rotating stall cell speed. The waves evolved smoothly into rotating stall without sharp changes in phase or amplitude, implying that, in the machines tested, the prestall waves and the fully developed rotating stall are two stages of the same phenomenon. The growth rate of these disturbances was in accord with that predicted by current analytical models. The prestall waves were observed both with uniform and with distorted inflow, but were most readily discerned with uniform inflow. Engineering uses and limitations of these waves are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleRotating Waves as a Stall inception Indication in Axial Compressors
typeJournal Paper
journal volume113
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929105
journal fristpage290
journal lastpage301
identifier eissn1528-8900
keywordsCompressors
keywordsWaves
keywordsStall inception
keywordsMachinery
keywordsInflow
keywordsMeasurement AND Travel
treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 002
contenttypeFulltext


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