Numerical investigation of influence of tip leakage flow on secondary flow in transonic centrifugal compressor at design condition

Author:

Kaneko Masanao,Tsujita Hoshio

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference5 articles.

1. M. Marconcini, 2008: Design and Off-Design Numerical Investigation of a Transonic Double-Splitter Centrifugal Compressor, Proceedings of ASME Turbo Expo 2008, Berlin, Germany, GT2008-50759.

2. Yamada K., 2007: The Behavior of Tip Clearance Flow at Near-Stall Condition in a Transonic Axial Compressor Rotor, Proceedings of ASME Turbo Expo 2007, Montreal, Canada, GT2007-27725.

3. C. Hah, 2006: Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor -Criteria and Mechanisms, Proceedings of ASME Turbo Expo 2006, Barcelona, Spain, GT2006-90045.

4. H. Krain, 2002: Investigations of the Flow Through a High Pressure Ratio Centrifugal Impeller, Proceedings of ASME Turbo Expo 2002, Amsterdam, the Netherlands, GT-2002-30394.

5. Ibaraki S., 2007: Vortical Flow Structure and Loss Generation Process in a Transonic Centrifugal Compressor Impeller, Proceedings of ASME Turbo Expo 2007, Montreal, Canada, GT2007-27791.

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