Intermittent Flow Regimes in a Transonic Fan Airfoil Cascade

A study was conducted in the NASA Glenn Research Center (NASA-GRC) linear cascade on the intermittent flow on the suction surface of an airfoil section from the tip region of a modern low aspect ratio fan blade. Experimental results revealed that, at a large incidence angle, a range of transonic inl...

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Bibliographic Details
Main Authors: J. Lepicovsky, E. R. McFarland, R. V. Chima, V. R. Capece, J. Hayden
Format: Article
Language:English
Published: Wiley 2004-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/S1023621X04000144
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