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Active Flow Control Stator With Coanda SurfaceActive Flow Control increases the permissible aerodynamic loading. Curved surface near the trailing edge ("Coanda surface"): a) increases turning -> higher pressure ratio. b) controls boundary layer separation -> increased surge margin. Objective: Reduce the number of vanes or compressor stages. Constraints: 1. In a real compressor, the vane must still function entirely without blowing. 2. Maintain the flow exit angle of the reference stator despite the resulting increase in stator loading.
Document ID
20100018562
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Guendogdu
(Leibniz Universitaet Hannover, Germany)
Vorreiter
(Leibniz Universitaet Hannover, Germany)
Seume
(Leibniz Universitaet Hannover, Germany)
Date Acquired
August 24, 2013
Publication Date
February 1, 2010
Publication Information
Publication: Minnowbrook VI: 2009 Workshop on Flow Physics and Control for Internal and External Aerodynamics
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Public Use Permitted.
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