Circumferential propagation of tip leakage flow unsteadiness for a low-speed axial compressor
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-009-0202-6.pdf
Reference10 articles.
1. Camp, T. R., Day, I. J., “A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor,” ASME J. Turbomachinery, Vol. 120, No. 3, 1998, pp. 393–401.
2. Vo, H. D., Tan, C. H. and Greitzer, E. M., “Criteria for Spike Initiated Rotating Stall,” ASME Paper GT 2005-68374, June 2005.
3. Hah, C., Bergner, J., and Schiffer, H. Z., “Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor-Criteria and Mechanism,” ASME Paper GT2006-90045, May 2006.
4. Mailach, R., Lehmann, I., and Vogeler, K., “Rotating Instability in an Axial Compressor Originating from the Fluctuating Blade Tip Vortex,” ASME Paper 2000-GT-506, May 2000.
5. März, J., Hah, C., and Neise, W., “An Experiment and Numerical Investigation into the Mechanisms of Rotating Instability,” ASME Paper 2001-GT-536, June 2001.
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