Effect of Recirculation Device With Counter Swirl Vane on Performance of High Pressure Ratio Centrifugal Compressor
Author:
Affiliation:
1. Turbo Machinery and Engine Technology Department, IHI Corporation, 1, Shin-Nakahara-Cho, Isogo-Ku, Yokohama, 235-8501
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4004820/5852966/051036_1.pdf
Reference18 articles.
1. Codan, E., and Mathey, C., 2007, “Emissions − A New Challenge for Turbochargers,” CIMAC Congress, Vienna, Paper No. 245.
2. Ibaraki, S., Furukawa, M., Iwakiri, K., and Takahashi, K., 2007, “Vortical Flow Structure and Loss Generation Process in a Transonic Centrifugal Compressor Impeller,” ASME Paper No. GT2007-27791.
3. Analysis of Vortical Flow Field in a Centrifugal Compressor Impeller with Vaneless Diffuser;Iwakiri
4. Guo, G., Zhang, Y., Xu, J., Zheng, X., and Zhuge, W., 2008, “Numerical Simulation of a Transonic Centrifugal Compressor Blade Tip Clearance Flow of Vehicle Turbocharger,” ASME Paper No. GT2008-50957.
5. Higashimori, H., Hasegawa, K., and Sumida, K., 2004, “Detailed Flow Study of Mach number 1.6 High Transonic Flow with a Shock Wave in a Pressure Ratio 11 Centrifugal Compressor Impeller,” ASME Paper No. GT2004-53435.
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