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International Journal of Rotating Machinery
Volume 2008, Article ID 657202, 10 pages
Research Article

Simulation of Casing Treatments of a Transonic Compressor Stage

1Institute for Flight Propulsion, Technische Universität München, Boltzmannstraße 15, 85747 Garching, Germany
2Compressor Aerodynamics, Rolls-Royce Deutschland, Eschenweg 11, 15827 Dahlewitz Berlin, Germany

Received 31 March 2008; Accepted 1 October 2008

Academic Editor: Chunill Hah

Copyright © 2008 M. Hembera et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. R. D. Moore, G. Kovich, and R. J. Blade, “Effect of casing treatment on overall and blade-element performance of a compressor rotor,” NASA TN D-6538, 1971.
  2. D. C. Prince, D. C. Wisler, and D. E. Hilvers, “Study of casing treatment stall margin improvement,” NASA CR-134552, 1974.
  3. H. Takata and Y. Tsukuda, “Stall margin improvement by casing treatment—its mechanism and effectiveness,” ASME Journal of Engineering for Power, vol. 99, no. 1, pp. 121–133, 1977. View at Google Scholar
  4. E. M. Greitzer, J. P. Nikkanen, D. E. Haddad, R. S. Mazzawy, and H. D. Joslyn, “A fundamental criterion for the application of rotor casing treatment,” ASME Journal of Fluids Engineering, vol. 101, no. 2, pp. 237–243, 1979. View at Google Scholar
  5. J. Paulon and D. Dehondt, “Influence of casing treatment on the operating range of axial compressors,” ASME Paper 82-GT-103, 1982.
  6. G. D. J. Smith and N. A. Cumpsty, “Flow phenomena in compressor casing treatment,” Journal of Engineering for Gas Turbines and Power, vol. 106, no. 3, pp. 532–541, 1984. View at Google Scholar
  7. A. R. Azimian, R. L. Elder, and A. B. McKenzie, “Application of recess vaned casing treatment to axial flow fans,” ASME Paper 89-GT-68, 1989.
  8. D. W. Thompson, P. I. King, and D. C. Rabe, “Experimental investigation of stepped tip gap effects on the performance of a transonic axial-flow compressor rotor,” ASME Paper 97-GT-7, 1997.
  9. M. D. Hathaway, “Self-recirculating casing treatment concept for enhanced compressor performance,” NASA TM-2002-211569, 2002.
  10. D. C. Rabe and C. Hah, “Application of casing circumferential grooves for improved stall margin in a transonic axial compressor,” ASME Paper GT-2002-30641, 2002.
  11. I. Wilke and H.-P. Kau, “A numerical investigation of the flow mechanisms in a HPC front stage with axial slots,” ASME Paper GT-2003-38481, 2003.
  12. I. Wilke, H.-P. Kau, and G. Brignole, “Numerically aided design of a high-efficient casing treatment for a transonic compressor,” ASME Paper GT2005-68993, 2005.
  13. G. Brignole, H.-P. Kau, and I. Wilke, “Numerical evaluation of important parameters ruling the effectiveness of casing treatments in transonic compressors,” ISABE Paper ISABE-2005-1095, 2005.
  14. X. Lu, W. Chu, J. Zhu, and Y. Wu, “Mechanism of the interaction between casing treatment and tip leakage flow in a subsonic axial compressor,” ASME Paper GT2006-90077, 2006.
  15. X. Lu, W. Chu, J. Zhu, and Y. Wu, “Experimental and numerical investigation of a subsonic compressor with bend skewed slot casing treatment,” ASME Paper GT2006-90026, 2006.
  16. M. W. Müler, H.-P. Schiffer, and C. Hah, “Effect of circumferential grooves on the aerodynamic performance of an axial single-stage transonic compressor,” ASME Paper GT2007-27365, 2007.
  17. W. Hofmann and J. Ballmann, “Tip clearance vortex development and shock-vortex-interaction in a transonic axial compressor rotor,” AIAA Paper 2002-0083, 2002.
  18. W. Hofmann and J. Ballmann, “Some aspects of tip vortex behavior in a transonic turbocompressor,” ISABE Paper ISABE-2003-1223, 2003.
  19. S. Schlechtriem and M. Lötzerich, “Breakdown of tip leakage vortices in compressors at flow conditions close to stall,” ASME Paper 97-GT-041, 1997.
  20. M. Furukawa, M. Inoue, K. Saiki, and K. Yamada, “The role of tip leakage vortex breakdown in compressor rotor aerodynamics,” ASME Paper 98-GT-239, 1998.
  21. M. Hoeger, G. Fritsch, and D. Bauer, “Numerical simulation of the shock-tip leakage vortex interaction in a HPC front stage,” ASME Paper 98-GT-261, 1998.
  22. I. Wilke and H.-P. Kau, “A numerical investigation of the flow mechanisms in a high pressure compressor front stage with axial slots,” Journal of Turbomachinery, vol. 126, no. 3, pp. 339–349, 2004. View at Publisher · View at Google Scholar
  23. I. Wilke and H.-P. Kau, “A numerical investigation of the influence of casing treatments on the tip leakage flow in a HPC front stage,” ASME-Paper GT-2002-20642, 2002.
  24. I. Wilke, Verdichterstabilisierung mit passive Gehäusestrukturierungen—eine numerische Analyse, Ph.D. dissertation, Institute of Flight Propulsion, Technische Universität München, Munich, Germany, 2005.