Closure to “Discussion of ‘Rotating Instabilities in an Axial Compressor Originating from the Fluctuating Blade Tip Vortex’ (2000-GT-506)” (2001, ASME J. Turbomach., 123, p. 461)

[+] Author and Article Information
Konrad Vogeler, Ronald Mailach, Ingolf Lehmann

Dresden University of Technology, Institute for Fluid Mechanics, 01062 Dresden, Germany

J. Turbomach 123(3), 461-463 (Jul 01, 2001) (3 pages) doi:10.1115/1.1374436 History:
Copyright © 2001 by ASME
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Day,  I. J., Breuer,  T., Escuret,  J., Cherett,  M., and Wilson,  A., 1999, “Stall Inception and the Prospects for Active Control in Four High-Speed Compressors,” ASME J. Turbomach., 121, pp. 18–27.
Inoue,  M., Kuroumaru,  M., Tanino,  T., and Furukawa,  M., 2000, “Propagation of Multiple Short Length-Scale Stall Cells in an Axial Compressor Rotor,” ASME J. Turbomach., 122, pp. 45–53.
Mathioudakis, K., and Breugelmans, F. A. E., 1985, “Development of Small Rotating Stall in a Single Stage Axial Compressor,” ASME Paper No. 85-GT-227.
Longley,  J. P., and Hynes,  T. P., 1990, “Stability of Flow Through Multistage Axial Compressors,” ASME J. Turbomach., 112, pp. 126–132.
Baumgartner, M., Kameier, F., and Hourmouziadis, J., 1995, “Non-Engine Order Blade Vibration in a High Pressure Compressor,” Proc. 12th International Symposium on Airbreathing Engines, Sept. 10–15, Melbourne, Australia.
Kameier, F., 1994, “Experimentelle Untersuchung zur Entstehung und Minderung des Blattspitzen-Wirbellärms axialer Strömungsmaschinen,” Fortschritt-Berichte VDI Reihe 7 No. 243, Düsseldorf, Germany.
Mailach, R., Sauer, H., and Vogeler, K., 2001, “The Periodical Interaction of the Tip Clearance Flow in the Blade Rows of Axial Compressors,” ASME Paper No. 2001-GT-0299.


Grahic Jump Location
Frequency spectrum with typical sign of a single-cell full-span rotating stall in Dresden LSRC (measured at the casing)
Grahic Jump Location
Signal of a pressure sensor on a rotor blade, sensor near blade tip (92 percent of channel height) and leading edge (10 percent of chord length), operating point near stability limit (design speed, ξ=0.82), tip clearance ratio s*=4.3 percent
Grahic Jump Location
Overview of the main unsteady flow phenomena in the stable operating range close to the stability limit of axial compressors




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