Browse > Article
http://dx.doi.org/10.5293/kfma..2011.15.1.052

Stall Inception Characteristics of Axial Compressor Varying IGV Stagger  

Bae, Hyo-Jo (서울대학교 기계항공공학부 대학원)
Lim, Hyung-Soo (서울대학교 기계항공공학부 대학원)
Song, Seung-Jin (서울대학교 기계항공공학부)
Kang, Shin-Hyoung (서울대학교 기계항공공학부)
Yang, Soo-Seok (한국항공우주연구원 첨단추진기관팀)
Publication Information
Abstract
Stall inception characteristics are researched to understand stall well. To realize different stall inception patterns, IGV stagger angle was changed. At design IGV stagger angle, spike, which is short length scale, is observed. Decreasing IGV stagger angle, spike changes to mode, which is long length scale, and further decreasing get multi cell. Compressor maps for each IGV stagger are shown to compare different stall inceptions. The characteristics of both spike and mode are confirmed in this experiment. Furthermore, transient from spike to mode is find. multi cell has 4cells and is little bit faster than mode. and multi cell shows 2nd, 3rd characteristics on compressor map.
Keywords
Axial compressor; Stall; Rotating stall; Stall inception; IGV; mode; spike; multi cell;
Citations & Related Records
연도 인용수 순위
  • Reference
1 강정식, 2002, "원심압축기의 스톨 발단에 관한 실험적 연구," 박사학위논문.
2 T. R. Camp and I. J. Day, 1998, "A Study of Spike and Modal Stall Phenomena in a Low Speed Axial Compressor," J. of Turbomachinery Vol. 120.
3 I. J. Day, 1993, "Stall Inception in Axial Flow Compressor," J. of Turbomachinery, Vol. 115.
4 N. M. Mcdougall, N. A. Cumpsty, and T. P. Hynes, 1990, "Stall Inception in Axial Compressor," J. of Turbomachinery, Vol. 112.
5 V. H. Garnier, A. H. Epstein, E. M. Greitzer, 1991, "Rotating Waves as a Stall Inception Indication in Axial compressor," J. of turbomachinery Vol. 113.
6 K. M. Boyer, P. I. King and W. W. Copengaver, 1993, "Stall Inception in Single-Stage High-Speed Compressors With Straight and Swept Leading Edges," AIAA Paper No. 93-1870.
7 M. Tryfonidis, O. Etchevers, J. D. Paduano, A. H. Epstein and G. J. Hendricks, 1995, "Prestall Behavior of Several High-Speed Compressors," J. of turbomachinery Vol. 117.
8 A. G. Wilson and C. Freeman, 1994, "Stall Inception and Development in Axial Flow Aeroengine," J. of Turbomachinery Vol. 116.
9 J. P. Longley, H. W. Shin, R. E. Plumley, P. D. Silkowski, I. J. Day, E. M. Greitzer, C. s. Tan and D. C. Wisler, 1996, "Effects of Rotating Inlet Distortion on Multistage Compressor Stability," J. of Turbomachinery Vol. 118.
10 B. Dobrzynski, H. Saathoff and G. Kosyna, 2007, "Influence of the Rotor Tip Stagger Angle on Axial Compressor Stall Inception," 7th ETC, Athens.
11 T. Houghton and I. J. Day, 2010, "Stability Enhancement by Casing Grooves : The Importance of Stall inception Mechanism and Solidity," Turboexpo 2010, GT2010-22284.
12 T. Kroeckel, S. J. Hiller and P. Jeschke, 2011, "Application of a Multistage Casing Treatment in a High Speed Axial Compressor Test Rig," Turboexpo 2011, GT2011-46315.