Injection profile effects on low speed axial compressor stability enhancement-Reference-Cited by-同舟云学术

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Injection profile effects on low speed axial compressor stability enhancement

Published:2011-06 Issue:6 Volume:25 Page:1501-1507
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Lim Hyung-Soo,Bae Hyo-Jo,Lim Young-Cheon,Song Seung-Jin,Kang Shin-Hyoung,Yang Soo-Seok

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/s12206-011-0332-0.pdf

Reference14 articles.

1. I. J. Day, Active suppression of rotating stall and surge in axial compressor, J. of Turbomachinery, 115 (1993) 40–47.

2. H. J. Weigl, J. D. Paduano, L. G. Frechette, A. H. Epstein, E. M. Greitzer, M. M. Bright and A. J. Strazisar, Active stabilization of rotating stall and surge in a transonic single stage axial compressor, J. of Turbomachinery, 120 (1998) 625–636.

3. K. L. Suder, M. D. Hathaway, S. A. Thorp, A. J. Strazisar and M. M. Bright, Compressor stability enhancement using discrete tip injection, Proc. of ASME Turbo Expo, Munich, Germany (2000) 2000-GT-650.

4. S. J. Strazisar, M. M. Bright, S. Thorp, D. E. Culley and K. L. Suder, Compressor stall control through endwall recirculation, Proc. of ASME Turbo Expo, Vienna, Austria (2004) GT2004-54295.

5. R. D. Andrea, R. L. Behnken and R. M. Murray, Rotating stall control of an axial flow compressor using pulsed air injection, J. of Turbomachinery, 119 (1997) 742–752.

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