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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| Format: | Article |
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ASME International
2018
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| Online Access: | http://hdl.handle.net/1721.1/116400 https://orcid.org/0000-0002-2343-910X https://orcid.org/0000-0001-9625-1020 https://orcid.org/0000-0002-8805-5289 |