Simulation of DBD plasma actuator effect on aerodynamic performance improvement using a modified phenomenological model

DOI10.1016/j.compfluid.2016.10.015zbMath1390.76926OpenAlexW2533432453MaRDI QIDQ1647189

Y. Aharonov

Publication date: 26 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2016.10.015

zbMATH Keywords

phenomenological modelflow separation controlwind turbine airfoilDBD plasma actuator

Mathematics Subject Classification ID

Packaged methods for numerical algorithms (65Y15) Ionized gas flow in electromagnetic fields; plasmic flow (76X05)

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Cites Work

• Utilizing the L-PSJA for controlling cylindrical wake flow
• Flow Control