Experimental cross-flow control in a 3D boundary layer by multi-discharge plasma actuators-Reference-Cited by-同舟云学术

Experimental cross-flow control in a 3D boundary layer by multi-discharge plasma actuators

Published:2021-05 Issue: Volume:112 Page:106643
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Baranov Sergey A.,Chernyshev Sergey L.,Khomich Vladislav Yu.,Kiselev Andrey Ph.,Kuryachii Aleksandr P.,Moshkunov Sergey I.^ORCID,Rebrov Igor E.,Sboev Dmitry S.,Tolkachev Stepan N.,Yamshchikov Vladimir A.

Funder

Ministry of Education and Science of the Russian Federation

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference50 articles.

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4. SDBD plasma enhanced aerodynamics: concepts, optimization and applications;Corke;Prog. Aerosp. Sci.,2007

5. Dielectric barrier discharge plasma actuators for flow control;Corke;Annu. Rev. Fluid Mech.,2010

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