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Abstract
For a high-pressure-ratio centrifugal compressor, the behavior of shock waves should be clarified to improve its performance. In the present paper, the flow including shock waves at the inducer of impeller is simulated using a commercial CFD code. Regarding the relative flow Mach number contours at the inducer, the flow structure including shock waves is discussed. And the results are compared with the experimental results by PIV. And it is shown that the agreement is fair.
Journal
- 年次大会講演論文集 : JSME annual meeting [List of Volumes]
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年次大会講演論文集 : JSME annual meeting 2006(2), 157-158, 2006-09-15 [Table of Contents]
The Japan Society of Mechanical Engineers