A Blockage Model for Centrifugal Compressor ImpellersSource: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004::page 698Author:R. C. Pampreen
DOI: 10.1115/1.3230792Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents and discusses the results of an analysis in which the blockage distributions of four impellers were deduced from shroud static pressure measurements. The purpose of the analysis was to provide a means of estimating blockage for the jet-wake flow model for use in impeller design calculations. A parameter was investigated for correlating the blockage values against the combined effect of diffusion, curvature, and Coriolis acceleration. It was found that gross blockage accumulation correlates against this parameter with an uncertainty in blockage of ± six percentage points. Up to the point of the axial-radial bend of the flowpath, the analysis shows that blockage is controlled equally by diffusion, flowpath curvature, and the combined effect of blade curvature and Coriolis acceleration. In the radial portion of the impeller, further increase in blockage is controlled by Richardson number.
keyword(s): Flow (Dynamics) , Diffusion (Physics) , Pressure measurement , Impellers , Wakes , Design , Blades , Compressor impellers AND Uncertainty ,
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contributor author | R. C. Pampreen | |
date accessioned | 2017-05-08T23:10:58Z | |
date available | 2017-05-08T23:10:58Z | |
date copyright | October, 1981 | |
date issued | 1981 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26769#698_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/94472 | |
description abstract | This paper presents and discusses the results of an analysis in which the blockage distributions of four impellers were deduced from shroud static pressure measurements. The purpose of the analysis was to provide a means of estimating blockage for the jet-wake flow model for use in impeller design calculations. A parameter was investigated for correlating the blockage values against the combined effect of diffusion, curvature, and Coriolis acceleration. It was found that gross blockage accumulation correlates against this parameter with an uncertainty in blockage of ± six percentage points. Up to the point of the axial-radial bend of the flowpath, the analysis shows that blockage is controlled equally by diffusion, flowpath curvature, and the combined effect of blade curvature and Coriolis acceleration. In the radial portion of the impeller, further increase in blockage is controlled by Richardson number. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | A Blockage Model for Centrifugal Compressor Impellers | |
type | Journal Paper | |
journal volume | 103 | |
journal issue | 4 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.3230792 | |
journal fristpage | 698 | |
journal lastpage | 707 | |
identifier eissn | 0742-4795 | |
keywords | Flow (Dynamics) | |
keywords | Diffusion (Physics) | |
keywords | Pressure measurement | |
keywords | Impellers | |
keywords | Wakes | |
keywords | Design | |
keywords | Blades | |
keywords | Compressor impellers AND Uncertainty | |
tree | Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004 | |
contenttype | Fulltext |