Modeling of Compressor Performance Deterioration Due to Erosion

This paper presents the results of a simulation of compressor performance deterioration due to blade erosion. The simulation at both design and off-design conditions is based on a mean line row by row model, which incorporates the effects of blade roughness and tip clearance. The results indicate a...

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Bibliographic Details
Main Authors: A. Hamed, W. Tabakoff, D. Singh
Format: Article
Language:English
Published: Hindawi Limited 1998-01-01
Series:International Journal of Rotating Machinery
Subjects:
Online Access:http://dx.doi.org/10.1155/S1023621X98000207
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spelling doaj-790be9b1e1ce4ca8acf8fa214cc866cc2020-11-24T22:19:44ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X1998-01-014424324810.1155/S1023621X98000207Modeling of Compressor Performance Deterioration Due to ErosionA. Hamed0W. Tabakoff1D. Singh2Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati 45221, OH, USADepartment of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati 45221, OH, USADepartment of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati 45221, OH, USAThis paper presents the results of a simulation of compressor performance deterioration due to blade erosion. The simulation at both design and off-design conditions is based on a mean line row by row model, which incorporates the effects of blade roughness and tip clearance. The results indicate a pronounced effect of blade erosion on the compressor adiabatic efficiency and a lesser effect on the pressure ratio. The loss in performance is mainly caused by the increased blade surface roughness and was highest at 100% speed.http://dx.doi.org/10.1155/S1023621X98000207CompressorPerformance deteriorationSimulationErosionRoughness.
collection DOAJ
language English
format Article
sources DOAJ
author A. Hamed
W. Tabakoff
D. Singh
spellingShingle A. Hamed
W. Tabakoff
D. Singh
Modeling of Compressor Performance Deterioration Due to Erosion
International Journal of Rotating Machinery
Compressor
Performance deterioration
Simulation
Erosion
Roughness.
author_facet A. Hamed
W. Tabakoff
D. Singh
author_sort A. Hamed
title Modeling of Compressor Performance Deterioration Due to Erosion
title_short Modeling of Compressor Performance Deterioration Due to Erosion
title_full Modeling of Compressor Performance Deterioration Due to Erosion
title_fullStr Modeling of Compressor Performance Deterioration Due to Erosion
title_full_unstemmed Modeling of Compressor Performance Deterioration Due to Erosion
title_sort modeling of compressor performance deterioration due to erosion
publisher Hindawi Limited
series International Journal of Rotating Machinery
issn 1023-621X
publishDate 1998-01-01
description This paper presents the results of a simulation of compressor performance deterioration due to blade erosion. The simulation at both design and off-design conditions is based on a mean line row by row model, which incorporates the effects of blade roughness and tip clearance. The results indicate a pronounced effect of blade erosion on the compressor adiabatic efficiency and a lesser effect on the pressure ratio. The loss in performance is mainly caused by the increased blade surface roughness and was highest at 100% speed.
topic Compressor
Performance deterioration
Simulation
Erosion
Roughness.
url http://dx.doi.org/10.1155/S1023621X98000207
work_keys_str_mv AT ahamed modelingofcompressorperformancedeteriorationduetoerosion
AT wtabakoff modelingofcompressorperformancedeteriorationduetoerosion
AT dsingh modelingofcompressorperformancedeteriorationduetoerosion
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