An Improved Integral Method for Prediction of Distorted Inlet Flow Propagation in Axial Compressor
An improved integral method is proposed and developed for the quantitative prediction of distorted inlet flow propagation through axial compressor. The novel integral method is formulated using more appropriate and practical airfoil characteristics, with less assumptions needed for derivation. The r...
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| Hauptverfasser: | , , , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
Wiley
2005-01-01
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| Schriftenreihe: | International Journal of Rotating Machinery |
| Schlagworte: | |
| Online-Zugang: | http://dx.doi.org/10.1155/IJRM.2005.117 |
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