• Title/Summary/Keyword: Pressure loss coeff.

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Performance Test and Aerodynamic Design on the High Pressure Ratio Centrifugal Compressor of a Turbocharger (과급기의 고압력비 원심압축기 공력설계 및 시험평가)

  • Kim, Hong-Won;Ryu, Seung-Hyup;Lee, Geun-Sik
    • The KSFM Journal of Fluid Machinery
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    • v.17 no.6
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    • pp.13-20
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    • 2014
  • It is necessary to design a compressor with high pressure ratio that satisfies the IMO(international maritime organization) NOx emission regulation for the marine diesel engine. Impeller was designed using the modified slip factor with the flow coefficient. The main purpose of this study is to investigate the sensitivity of the compressor performance by the vaned diffuser geometries. The first vaned diffuser type was based on a NACA airfoil, the second was channel diffuser, and the third was conformally transformated configuration of a NACA65(4A10)06 airfoil. The sensitivity of the performance was calculated using a commercial CFD program for three different diffuser geometries. The channel diffuser showed the wide range of operation and higher pressure characteristics, comparing with the others. This is attributed to the flow stability at diffuser. Combined with this results with impeller design, the optimized compressor was designed and verified by the test results.