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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Grahic Jump Location
Overview of the main unsteady flow phenomena in the stable operating range close to the stability limit of axial compressors
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
Frequency spectrum with typical sign of a single-cell full-span rotating stall in Dresden LSRC (measured at the casing)




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