Show simple item record

contributor authorI. J. Day
date accessioned2017-05-08T23:42:55Z
date available2017-05-08T23:42:55Z
date copyrightJanuary, 1993
date issued1993
identifier issn0889-504X
identifier otherJOTUEI-28627#1_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112841
description abstractStudies have been conducted on two laboratory test compressors to investigate the process leading to the formation of finite amplitude rotating stall cells. The measurements were obtained from circumferential arrays of hot wires and were spatially and temporarily analyzed to show that modal perturbations are not always present prior to stall, and when present, sometimes have little direct effect on the formation of the stall cells. The measurements lead to the conclusion that the occurrence of modal perturbations, and the formation of finite amplitude stall cells, are two separate phenomena, both occurring under roughly the same conditions at the peak of the pressure rise characteristic. The measurements also underline the hitherto unsuspected importance of short length scale disturbances in the process of stall inception. Examples are given of different ways in which stall cells can develop and the conclusions are backed up with a summary of current test data from various machines around the world.
publisherThe American Society of Mechanical Engineers (ASME)
titleStall Inception in Axial Flow Compressors
typeJournal Paper
journal volume115
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929209
journal fristpage1
journal lastpage9
identifier eissn1528-8900
keywordsCompressors
keywordsAxial flow
keywordsStall inception
keywordsMeasurement
keywordsWire
keywordsPressure AND Machinery
treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record