Unsteady tip clearance flow pattern in an isolated axial compressor rotor with micro tip injection
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-007-0309-6.pdf
Reference20 articles.
1. Vo, H. D., Tan, C. H., and Greitzer, E. M., “Criteria for Spike Initiated Rotating Stall”, ASME Paper 2005-GT-68374
2. Hah, C., Bergner, J., and Schiffer, H. Z., “Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor-Criteria and Mechanism”, ASME Paper 2006-GT-90045
3. Rabe, D. C., and Hah, C., “Application of Casing Circumferential Grooves for Improved Stall Margin in a Transonic Axial Compressor”, ASME Paper 2002-GT-30641
4. Shabbir, A., and Adamczyk, J. J., “Flow Mechanism for Stall Margin Improvement due to Circumferential Casing Grooves on Axial Compressors”, ASME J. Turbomachinery, 2005, Vol. 127, pp. 708–717
5. Suder, K. L., Hathaway, M. D., Thorp, S. A., Strazisar, A. J., and Bright, M. B., “Compressor Stability Enhancement Using Discrete Tip Injection”, ASME J. Turbomachinery, 2001, Vol. 123, pp. 14–23
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