Stall Inception in Axial Flow CompressorsSource: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001::page 1Author:I. J. Day
DOI: 10.1115/1.2929209Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Studies 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.
keyword(s): Compressors , Axial flow , Stall inception , Measurement , Wire , Pressure AND Machinery ,
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contributor author | I. J. Day | |
date accessioned | 2017-05-08T23:42:55Z | |
date available | 2017-05-08T23:42:55Z | |
date copyright | January, 1993 | |
date issued | 1993 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28627#1_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/112841 | |
description abstract | Studies 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Stall Inception in Axial Flow Compressors | |
type | Journal Paper | |
journal volume | 115 | |
journal issue | 1 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2929209 | |
journal fristpage | 1 | |
journal lastpage | 9 | |
identifier eissn | 1528-8900 | |
keywords | Compressors | |
keywords | Axial flow | |
keywords | Stall inception | |
keywords | Measurement | |
keywords | Wire | |
keywords | Pressure AND Machinery | |
tree | Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001 | |
contenttype | Fulltext |