Performance Limits of Axial Compressor Stages
This paper presents a framework for estimating the upper limit of compressor stage efficiency. Using a compressor stage model with a representative design velocity distribution with turbulent boundary layers, losses are calculated as the sum of selected local irreversibilities, rather than from corr...
Main Authors: | , , |
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Other Authors: | , |
Format: | Article |
Language: | English |
Published: |
ASME International,
2018-06-19T13:51:23Z.
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Subjects: | |
Online Access: | Get fulltext |