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contributor authorR. H. Aungier
date accessioned2017-05-08T23:48:35Z
date available2017-05-08T23:48:35Z
date copyrightJuly, 1995
date issued1995
identifier issn0889-504X
identifier otherJOTUEI-28645#360_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116131
description abstractAerodynamic Performance prediction models for centrifugal compressor impellers are presented. In combination with similar procedures for stationary components, previously published in the open literature, a comprehensive mean streamline performance analysis for centrifugal compressor stages is provided. The accuracy and versatility of the overall analysis is demonstrated for several centrifugal compressor stages of various types, including comparison with intrastage component performance data. Detailed validation of the analysis against experimental data has been accomplished for over a hundred stages, including stage flow coefficients from 0.009 to 0.15 and pressure ratios up to about 3.5. Its application to turbocharger stages includes pressure ratios up to 4.2, but with test uncertainty much greater than for the data used in the detailed validation studies.
publisherThe American Society of Mechanical Engineers (ASME)
titleMean Streamline Aerodynamic Performance Analysis of Centrifugal Compressors
typeJournal Paper
journal volume117
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2835669
journal fristpage360
journal lastpage366
identifier eissn1528-8900
keywordsCompressors
keywordsPressure
keywordsFlow (Dynamics)
keywordsCompressor impellers AND Uncertainty
treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 003
contenttypeFulltext


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