A Study on Flow Instability in an Axial Compressor of Gas Turbine for Power Generation at Partial-Load Conditions
Author:
Affiliation:
1. Energy Solution & Marine Engineering Company, Kawasaki Heavy Industries, Ltd.
2. Aerospace System Company, Kawasaki Heavy Industries, Ltd.
3. Corporate Technology Division, Kawasaki Heavy Industries, Ltd.
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/4/15_vol15no4tp04/_pdf
Reference27 articles.
1. Day, I. J. " Stall, Surge, and 75 Years of Research." ASME. J. Turbomach. January 2016; 138(1): 011001.
2. Fiquet, A., Aubert, S., Brandstetter, C., Buffaz, N., and Vercoutter, A. " Acoustic Resonance in an Axial Multistage Compressor Leading to Non-Synchronous Blade Vibration." ASME. J. Turbomach. September 2021; 143(9): 091014.
3. Inoue, M., Kuroumaru, M., Tanino, T., Yoshida, S., and Furukawa, M., 2001. “Comparative Studies on Short and Long Length-scale Stall Cell Propogating in an Axial Compressor Rotor”. ASME IGTI 2000-GT-506; ASME J. Turbomach. 123(3).
4. Yamada, K., Kikuta, H., Iwakiri, K., Furukawa, M., and Gunjishima, S. " An Explanation for Flow Features of Spike- Type Stall Inception in an Axial Compressor Rotor." ASME. J. Turbomach. March 2013; 135(2): 021023.
5. Yamada, K., Furukawa, M., Tamura, Y., Saito, S., Matsuoka, A., and Nakayama, K. " Large-Scale Detached-Eddy Simulation Analysis of Stall Inception Process in a Multistage Axial Flow Compressor." ASME. J. Turbomach. July 2017; 139(7): 071002.
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