| Autor: |
L. Fottner, D. K. Hennecke, W. M. König |
| Rok vydání: |
1994 |
| Předmět: |
|
| Zdroj: |
Volume 1: Turbomachinery. |
| DOI: |
10.1115/94-gt-335 |
| Popis: |
New blading concepts as used in modern transonic axial-flow compressors require improved loss and deviation angle correlations. The new model presented in this paper incorporates several elements and treats separately blade-row flows having subsonic and supersonic inlet conditions. The second part of the present report focuses on the extension of a well-known correlation for cascade losses at supersonic inlet-flows. It was originally established for DCA-bladings and is now modified to reflect the flow situation in blade-rows having low-cambered, arbitrarily designed blades including precompression blades. Finally, the steady loss increase from subsonic to supersonic inlet-flow velocities demonstrates the matched performance of the different correlations of the new model.Copyright © 1994 by ASME |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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