Experimental Evaluation of a High-Gain Control for Compressor Surge Suppression
Author:
Affiliation:
1. University of Udine, Dipartimento di Matematica e Informatica, Udine, Italy
2. University of Udine, Dipartimento di Energetica e Macchine, Udine, Italy
3. University of Trieste, Dipartimento di Energetica, Trieste, Italy
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/124/1/27/5756009/27_1.pdf
Reference24 articles.
1. Greitzer, E. M. , 1976, “Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System Model,” ASME J. Eng. Power, 98, pp. 190–198.
2. Moore, F. K., and Greitzer, E. M., 1986, “A Theory of Post-Stall Transients in Axial Compression Systems: Part I—Development of Equations,” ASME J. Eng. Gas Turbines Power, 108, pp. 68–76.
3. Epstein, A. H., Ffowcs Williams, J. E., and Greitzer, E. M., 1989, “Active Suppression of Aerodynamic Instabilities in Turbomachines,” J. Propul. Power, 5, No. 2, pp. 204–211.
4. Ffowcs Williams, J. E., and Huang, X., 1989, “Active Stabilization of Compressor Surge,” J. Fluid Mech., 204, pp. 245–262.
5. Pinsley, L. E., Guenette, G. R., Epstein, A. H., and Greitzer, E. M., 1991, “Active Stabilization of Centrifugal Compressor Surge,” ASME J. Turbomach., 113, pp. 723–732.
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