Numerical analysis of the tip leakage flow field in a transonic axial compressor with circumferential casing treatment
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-010-0198-y.pdf
Reference10 articles.
1. Yamada K., Funazaki K. and Furukawa M. The Behavior of Tip Clearance Flow at Near-Stall Condition in a Transonic Axial Compressor Rotor, Proceedings of ASME Turbo Expo, Montreal, Canada, paper 2007-27725, 2007.
2. Hofman, W., and Ballmann, J. Tip Clearance Vortex Development and Shock-Vortex Interaction in a Transonic Axial Compressor Rotor. AIAA 2002-0083, Reno, Nevada, 2002.
3. Hoeger, M., Fritsch, G., and Bauer, D. Numerical Simulation of the Shock Tip Leakage Vortex Interaction in a HPC-Front Stage. ASME J. Turbomachinery, 120, pp. 131–140, 1998.
4. Wilke I., Kau H.-P. and Grignole G. Numerically aided Design of a High-Efficient Casing Treatment for a Transonic Compressor. Proceedings of ASME Turbo Expo 2005, Reno, Nevada, paper GT2005-68993, 2005.
5. Hathaway M. Self-Recirculating Casing Treatment Concept for Enhanced Compressor Performance. Proceedings of ASME Turbo Expo 2002, Amsterdam, paper GT2002-30368, 2002.
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