The Proceedings of Conference of Tohoku Branch
Online ISSN : 2424-2713
2008.43
Session ID : 122
Conference information
122 The influence that the tip leakage flow of an axial compressor for aeroengines gives to aerodynamics performance
Ken-ichi FUNAZAKI, Kazutoyo YAMADA, Hideo TANIGUCHI, Mamoru KIKUCHI, Katsuya SASAKI, Jun TANEICHI
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Keywords: Tip leakage flow, Tip clearance, Low Reynolds Number, Total Pressure Loss
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© 2008 The Japan Society of Mechanical Engineers
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