contributor author | J. P. Longley | |
contributor author | T. P. Hynes | |
date accessioned | 2017-05-08T23:34:11Z | |
date available | 2017-05-08T23:34:11Z | |
date copyright | January, 1990 | |
date issued | 1990 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28600#126_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107795 | |
description abstract | This paper describes measurements of the performance of a research stage operating in isolation and as part of a multistage compressor. It is shown that the stall point and the stalled performance of the stage are properties of the system in which it operates rather than a property of the stage itself. The consequences of this for the estimation of the stall point for compressors and compression systems are discussed. The support that the measurements give to assumptions made by mathematical models which use the concept of an “underlying axisymmetric” characteristic, are highlighted. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Stability of Flow Through Multistage Axial Compressors | |
type | Journal Paper | |
journal volume | 112 | |
journal issue | 1 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2927409 | |
journal fristpage | 126 | |
journal lastpage | 132 | |
identifier eissn | 1528-8900 | |
keywords | Stability | |
keywords | Flow (Dynamics) | |
keywords | Compressors | |
keywords | Measurement AND Compression | |
tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001 | |
contenttype | Fulltext | |