Comparison between synthetic jets and continuous jets for active flow control: Application on a NACA 0015 and a compressor stator cascade
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Published:2015-06
Issue:
Volume:43
Page:256-280
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ISSN:1270-9638
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Container-title:Aerospace Science and Technology
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language:en
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Short-container-title:Aerospace Science and Technology
Author:
De Giorgi M.G.,
De Luca C.G.,
Ficarella A.ORCID,
Marra F.
Subject
Aerospace Engineering
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4. Effect of a micro dielectric barrier discharge plasma actuator on quiescent flow;Pescini;IET Sci. Meas. Technol.,2014
5. M.G. De Giorgi, F. Marra, E. Pescini, A. Ficarella, Experimental and numerical analysis of a micro plasma actuator for active flow control in turbomachinery, in: Proceedings of the ASME Turbo Expo 2014, GT2014-25337, 2A:V02AT37A011.
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