Journal of Engineering and Applied Sciences
Year:
2016
Volume:
11
Issue:
12
Page No.
2769 - 2774
Effect of Blade Tip Geometry on Centrifugal Compressor Performance and Stability
Authors :
IbrahimShahin
References
Barton, M.T., M.L. Mansour, J.S. Liu and D.L. Palmer, 2006. Numerical optimization of a vaned shroud design for increased operability margin in modern centrifugal compressors. J. Turbomach., 128: 627-631.
CrossRef | Direct Link | Dickmann, H.P., T.S. Wimmel, J. Szwedowicz, D. Filsinger and C.H. Roduner, 2005. Unsteady flow in a turbocharger centrifugal compressor: 3D-CFD-simulation and numerical and experimental analysis of impeller blade vibration. Proceeding of the ASME Turbo Expo 2005: Power for Land, Sea and Air, June 6-9, 2005, American Society of Mechanical Engineers, Reno, Nevada, ISBN:0-7918-4730-6, pp: 1309-1321.
Farge, T.Z., M.W. Johnson and T.M.A. Maksoud, 1989. Tip leakage in a centrifugal impeller. J. Turbomach., 111: 244-249.
CrossRef | Direct Link | Furukawa, M., M. Inoue, K. Saiki and K. Yamada, 1998. The role of tip leakage vortex breakdown in compressor rotor aerodynamics. Proceeding of the ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition, June 2-5, 1998, American Society of Mechanical Engineers, Stockholm, Sweden, ISBN:978-0-7918-7862-0, pp: 14-14.
Hah, C., 1986. A numerical modeling of endwall and tip-clearance flow of an isolated compressor rotor. J. Eng. Gas Turbines Power, 108: 15-21.
CrossRef | Direct Link | Halawa, T., M. Alqaradawi, M.S. Gadala, I. Shahin and O. Badr, 2015. Numerical investigation of rotating stall in centrifugal compressor with vaned and vaneless diffuser. J. Therm. Sci., 24: 323-333.
CrossRef | Direct Link | Inoue, M., M. Kuroumaru and M. Fukuhara, 1986. Behavior of tip leakage flow behind an axial compressor rotor. J. Eng. Gas Turbines Power, 108: 7-14.
CrossRef | Direct Link | Ishida, M., D. Sakaguchi and H. Ueki, 2005. Optimization of inlet ring groove arrangement for suppression of unstable flow in a centrifugal impeller. Proceeding of the ASME Turbo Expo 2005: Power for Land, Sea and Air, June 6-9, 2005, American Society of Mechanical Engineers, Reno, Nevada, ISBN:0-7918-4730-6, pp: 841-850.
Ishida, M., H. Ueki and Y. Senoo, 1990. Effect of blade tip configuration on tip clearance loss of a centrifugal impeller. J. Turbomach., 112: 14-18.
CrossRef | Direct Link | Lakshminarayana, B., 1970. Methods of predicting the tip clearance effects in axial flow turbomachinery. J. Basic Eng., 92: 467-480.
CrossRef | Direct Link | Larosiliere, L.M. and G.J. Skoch, 1999. Aerodynamic synthesis of a centrifugal impeller using computational fluid dynamics and measurements. J. Propul. Power, 15: 623-632.
Direct Link | Larosiliere, L.M., G.J. Skoch and P.S. Prahst, 1997. Aerodynamic Synthesis of a Centrifugal Impeller Using CFD and Measurements. National Aeronautics and Space Administration, Seattle, Washington, USA.,.
McKain, T.F. and G.J. Holbrook, 1997. Coordinates for a High Performance 4: 1 Pressure Ratio Centrifugal Compressor. NASA, Indianapolis, Indiana, Pages: 82.
Moore, J., J.G. Moore and P.H. Timmis, 1984. Performance evaluation of centrifugal compressor impellers using three-dimensional viscous flow calculations. J. Eng. Gas Turbines Power, 106: 475-481.
CrossRef | Direct Link | Myong, H.K. and S.Y. Yang, 2003. Numerical study on flow characteristics at blade passage and tip clearance in a linear cascade of high performance turbine blade. KSME Int. J., 17: 606-616.
CrossRef | Direct Link | Shahin, I., M. Gadala, M. Alqaradawi and O. Badr, 2014. Unsteady CFD simulation for high speed centrifugal compressor operating near surge. Proceeding of the ASME Turbo Expo 2014: Turbine Technical Conference on Exposition, June 16-20, 2014, American Society of Mechanical Engineers, Dusseldorf, Germany, ISBN:978-0-7918-4563-9, pp: 10-10.
Shahin, I., M. Gadala, M. Alqaradawi and O. Badr, 2015. Large eddy simulation for a deep surge cycle in a high-speed centrifugal compressor with vaned diffuser. J. Turbomach., Vol. 137, 10.1115/1.4030790
Skoch, G.J., PS. Prahst, M.P. Wernet, J.R. Wood and A.J. Strazisar, 1997. Laser anemometer measurements of the flow field in a 4: 1 pressure ratio centrifugal impeller. Proceeding of the ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition, June 2-5, 1997, American Society of Mechanical Engineers, Orlando, Florida, ISBN:978-0-7918-7868-2, Pages:13-13.