0
TECHNICAL PAPERS

Aerodynamics of a Transonic Centrifugal Compressor Impeller

[+] Author and Article Information
Seiichi Ibaraki, Tetsuya Matsuo, Hiroshi Kuma, Kunio Sumida, Toru Suita

Nagasaki R&D Center, Mitsubishi Heavy Industries, Ltd., Nagasaki, 851-0392, Japan

J. Turbomach 125(2), 346-351 (Apr 23, 2003) (6 pages) doi:10.1115/1.1540117 History: Received January 25, 2002; Online April 23, 2003
Copyright © 2003 by ASME
Your Session has timed out. Please sign back in to continue.

References

Rodger, C., 1998, “The Centrifugal Compressor Inducer,” ASME Paper No. 98-GT-32.
Pak, H., Krain, H., and Hoffman, B., 1993, “Flow Field Analysis in a High Pressure Ratio Centrifugal Compressor,” AGARD Meeting.
Krain, H., Hoffman, B., and Pak, H., 1995, “Aerodynamics of a Centrifugal Compressor Impeller with Transonic Inlet Conditions,” ASME Paper No. 95-GT-97.
Eisenlohr, G., Dalbert, P., Krain, H., Proll, H., Richter, F., and Rohne, K., 1998, “Analysis of the Transonic Flow at the Inlet of a High Pressure Ratio Centrifugal Impeller,” ASME Paper No. 98-GT-24.
Krain, H., Karpinski, G., and Beversdorff, M., 2001, “Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-Component Laser Velocimetry,” ASME Paper No. 2001-GT-0315.
Ibaraki, S., Higashimori, H., and Matsuo, T., 2001, “Flow Investigation, of a Transonic Centrifugal Compressor for Turbocharger,” 23rd CIMAC.
Hayami, H., Umemoto, A., Itoh, K. and Kawaguchi, N., 1995, “Effects of Camber of Inducer on the Performance of a Transonic Centrifugal Compressor,” ASME FED-Vol. 222, Fluid Machinery.
Hah, C., and Krain, H., 1999, “Analysis of Transonic Flow Fields Inside a High Pressure Ratio Centrifugal Compressor at Design and Off Deign Conditions,” ASME Paper No. 99-GT-446.
Furukawa, M., Inoue, M., Saiki, K. and Yamada, K., 1998, “The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics,” ASME Paper No. 98-GT-239.
Dawes, W. N., 1987, “Application of a Three-Dimensional Viscous Compressible Flow Solver to a High-Speed Centrifugal Compressor Rotor—Secondary Flow and Loss Generation,” I Mech E Conf. Publ., No. C261/87.
Baldwin, B., and Lomax, H., 1978, “Thin Layer Approximation and Algebratic Model for Separated Turbulent Flows,” AIAA Pap., No. 78–257.

Figures

Grahic Jump Location
Cross section of test compressor
Grahic Jump Location
Meridional view of test impeller showing measurement locations
Grahic Jump Location
Compressor stage characteristics
Grahic Jump Location
Comparison of isentropic Mach number distribution of casing surface
Grahic Jump Location
Comparison of meridional velocity distribution at five sections
Grahic Jump Location
Comparison of pitchwise relative velocity distribution at four stations
Grahic Jump Location
Vortex cores colored with normalized helicity distribution
Grahic Jump Location
Vortex cores and tip leakage flow with stagnation pressure distributions

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In