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contributor authorCourtiade, Nicolas
contributor authorOttavy, Xavier
date accessioned2017-05-09T01:03:57Z
date available2017-05-09T01:03:57Z
date issued2013
identifier issn0889-504X
identifier otherturb_135_06_061018.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153531
description abstractPressure measurements using high frequency response sensors have been carried out on the third rotor of the 3.5stage high speed compressor CREATE (rotation speed: 11,543 RPM, Rotor 1 tip speed: 313 m/s) over the complete characteristic line and during the surge transient. Precursors to the instabilities occurring near surge are observable at stable operating points. Just before surge, these precursors characterized as rotating disturbances grow in amplitude and provoke the onset a stall cell after a variable duration, which finally triggers surge. This paper presents a detailed analysis of the phenomena of rotating instabilities and surge transient and shows that it is possible to develop an antisurge active control system based on the early detection of the precursors.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperimental Study of Surge Precursors in a High Speed Multistage Compressor
typeJournal Paper
journal volume135
journal issue6
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4023462
journal fristpage61018
journal lastpage61018
identifier eissn1528-8900
treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 006
contenttypeFulltext


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