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International Journal of Rotating Machinery
Volume 2012 (2012), Article ID 402763, 12 pages
The Mechanical Impact of Aerodynamic Stall on Tunnel Ventilation Fans
1Fläkt Woods Ltd., Axial Way, Colchester CO4 5ZD, UK
2Dipartimento di Ingegneria Meccanica e Aerospaziale, Sapienza University of Rome, Via Eudossiana 18, Rome 00184, Italy
Received 28 August 2011; Revised 3 December 2011; Accepted 7 December 2011
Academic Editor: Ting Wang
Copyright © 2012 A. G. Sheard and A. Corsini. 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.
- A. Rippl, Experimentelle untersuchungen zuminstationaren betriebsverhahen an der stabilitarsgrenze eines mehrstufigen transsonischen verdichters, Ph.D. dissertation, Ruhr-Universität Bochum, 1995.
- S. K. Ivanov, “Axial blower,” Patent No. US 3,189,260, 1965.
- J. T. Gravdahl and O. Egeland, Compressor Surge and Rotating Stall: Modeling and Control, Springer, London, UK, 1999.
- I. J. Day and N. A. Cumpsty, “The measurement and interpretation of flow within rotating stall cells in axial compressors,” Journal of Mechanical Engineering Science, vol. 20, pp. 101–114, 1978.
- E. M. Greitzer, “Review—axial compressor stall phenomena,” Transactions of the ASME, Journal of Fluids Engineering, vol. 102, no. 2, pp. 134–151, 1980.
- F. K. Moore, “A theory of rotating stall of multistage axial compressors: parts I–III,” Transactions of the ASME, Journal of Engineering for Gas Turbines and Power, vol. 106, no. 2, pp. 313–336, 1984.
- H. W. Emmons, C. E. Pearson, and H. P. Grant, “Compressor surge and stall propagation,” Transactions of the ASME, vol. 77, pp. 455–469, 1955.
- N. A. Cumpsty, “Part-circumference casing treatment and the effect on compressor stall,” ASME Paper No. 89-GT, 1989.
- S. Bianchi, A. Corsini, and A. G. Sheard, “Detection of stall regions in a low-speed axial fan. — part i: azimuthal acoustic measurements,” in Proceedings of the 54th American Society of Mechanical Engineers Turbine and Aeroengine Congress, vol. 3, pp. 169–179, Glasgow, UK, June 2010.
- A. G. Sheard, A. Corsini, and S. Bianchi, “Method of detecting stall in an axial fan,” Patent No. GB 2 468 571 B, 2010.
- A. G. Sheard, A. Corsini, and S. Bianchi, “Stall warning in a low-speed axial fan by visualization of sound signals,” Journal of Engineering for Gas Turbines and Power, vol. 133, no. 4, Article ID 041601, pp. 1–10, 2011.
- C. C. Koch and L. H. Smith, “Loss sources and magnitudes in axial-flow compressors,” Transactions of the ASME, Journal of Engineering and Power, vol. 98, no. 3, pp. 411–424, 1976.
- H. Saathoff and U. Stark, “Tip clearance flow induced endwall boundary layer separation in a single-stage axial-flow low-speed compressor,” ASME Paper No. 2000-GT-0501, 2000.
- S. A. Khalid, A. S. Khalsa, I. A. Waitz et al., “Endwall blockage in axial compressors,” Transactions of the ASME, Journal of Turbomachinery, vol. 121, no. 3, pp. 499–509, 1999.
- H. Vo, C. S. Tan, and E. M. Greitzer, “Criteria for spike initiated rotating stall,” ASME Paper GT 2005-68374, ASME Turbo Expo, Reno-Tahoe, Nevada, Nev, USA, 2005.
- M. M. Bright, H. Qammar, H. Vhora, and M. Schaffer, “Rotating pip detection and stall warning in high-speed compressors using structure function,” in Proceedings of AGARD RTO AVT Conference, Toulouse, France, May 1998.
- T. R. Camp and I. J. Day, “A study of spike and modal stall phenomena in a low-speed axial compressor,” Journal of Turbomachinery, vol. 120, no. 3, article 393, 9 pages, 1998.
- A. Deppe, H. Saathoff, and U. Stark, “Spike-type stall inception in axial flow compressors,” in Proceedings of the 6th Conference on Turbomachinery, Fluid Dynamics and Thermodynamics, Lille, France, 2005.
- M. D. Hathaway, “Passive endwall treatments for enhancing stability,” Report NASA/TM-2007-214409, 2007.
- G. L. Wilde, “Improvements in or relating to gas turbines,” Patent No. 701,576, 1950.
- R. C. Turner, “Improvements in or relating to gas turbines,” Patent No. 826,669, 1955.
- R. G. Griffin and L. H. Smith Jr., “Experimental evaluation of outer case blowing or bleeding of a single stage axial flow compressor, part I—design of rotor blowing and bleeding configurations,” NASA Report CR-54587, 1966.
- E. E. Bailey and C. H. Voit, Some observations of effects of porous casings on operating range of a single axial-flow compressor rotor. Report NASA-TM-X-2120, 1970.
- D. C. Prince, D. D. Wisler, and D. E. Hilvers, “Study of casing treatment stall margin improvement phenomena,” NASA Report CR-134552, 1974.
- D. C. Wisler and D. E. Hilvers, “Stator hub treatment study,” NASA Report CR-134729, 1974.
- H. Takata and Y. Tsukuda, “Stall margin improvement by casing treatment—its mechanism and effectiveness,” Journal of Engineering for Power, vol. 99, no. 1, article 121, 13 pages, 1977.
- 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,” Journal of Fluids Engineering, Transactions of the ASME, vol. 101, no. 2, pp. 237–243, 1979.
- S. G. Koff, R. S. Mazzawy, J. P. Nikkanen, and A. Nolcheff, “Case treatment for compressor blades,” Patent No. US 5,282,718, 1994.
- S. J. Khalid, “Compressor endwall treatment,” Patent No. US 5,520,508, 1996.
- N. A. Nolcheff, “Flow aligned plenum endwall treatment for compressor blades,” Patent No. US 5,586,859, 1996.
- F. S. Gelmedov, E. A. Lokshtanov, L. E.-M. Olstain, and M. A. Sidorkin, “Anti-stall tip treatment means,” Patent No. US 5,762,470, 1998.
- S. Karlsson and T. Holmkvist, “Guide vane ring for a return flow passage in axial fans and a method of protecting it,” Patent No. US 4,602,410, 1986.
- H. Bard, “The stabilization of axial fan performance,” in Proceedings of the Institution of Mechanical Engineers Conference C120/84 on the Installation Effects in Ducted Fan Systems (IMechE '84), pp. 100–106, 1984.
- Y. Miyake and T. Inaba, “Improvement of axial flow fan characteristics by means of separators,” Journal of Turbomachinery Society of Japan, vol. 13, pp. 746–752, 1985.
- N. Yamaguchi, M. Ogata, and Y. Kato, “Improvement of stalling characteristics of an axial-flow fan by radial vaned air separators,” Journal of Turbomachinery, vol. 132, no. 2, Article ID 021015, 10 pages, 2010.
- C. S. Kang, A. B. McKenzie, and R. L. Elder, “Recessed casing treatment effects on fan performance and flow field,” ASME Paper No. GT-95-197, 1995.
- A. G. Sheard, A. Corsini, S. Minotti, and F. Sciulli, “The role of computational methods in the development of an aero-acoustic design methodology: application in a family of large industrial fans,” in Proceedings of the 14th International Conference on Modelling Fluid Flow Technologies, pp. 71–79, Budapest, Hungary, September 2009.
- C. A. Wasserbauer, H. F. Weaver, and R. G. Senyitko, “NASA low-speed axial compressor for fundamental research,” NASA Technical Memorandum 4635, 1995.
- W. C. Young, Roark’s Formulas for Stress and Strain, McGraw-Hill, New York, NY, USA, 1989.
- W. Z. Gerber, “Calculation of the allowable stresses in iron structures,” Bayer Architecture & Engineering, vol. 6, pp. 101–110, 1874.