Performance Limits of Axial Compressor Stages

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...

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Bibliographic Details
Main Authors: Hall, David Kenneth (Contributor), Greitzer, Edward M (Contributor), Tan, Choon S (Contributor)
Other Authors: MIT-SUTD Collaboration (Contributor), Massachusetts Institute of Technology. Department of Aeronautics and Astronautics (Contributor)
Format: Article
Language:English
Published: ASME International, 2018-06-19T13:51:23Z.
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