Experimental Investigation of the Compressor Cascade under an Active Flow Control

The paper is concerned with flow past compressor blade cascade (NACA 65 with thickened trailing edge) at off-design regimes, which are characteristic by partial or complete flow separation on the suction surface of the blades. An attempt has been made to moderate the flow separation using continuous...

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Bibliographic Details
Main Authors: Lukáč J., Luxa M., Šimurda D., Cyrus V., Trávníček Z., Kordík J.
Format: Article
Language:English
Published: EDP Sciences 2013-04-01
Series:EPJ Web of Conferences
Online Access:http://dx.doi.org/10.1051/epjconf/20134501086