This study is focused on the active flow control in the internal flow of turbo-jet engines by Dielectric Barrier Discharges Actuators. In particular the application of this techniques has been studied with the aim of improving the aerodynamic behavior of compressor blades by reducing, or even eliminating, flow separation. A numerical electrostatic model has been implemented in the CFD code, to investigate the aerodynamic behaviour of a transonic compressor rotor with and without plasma actuators.

ACTIVE FLOW CONTROL USING PLASMA ACTUATORS IN GAS TURBINE ENGINE

DE GIORGI, Maria Grazia;TRAFICANTE, STEFANIA;FICARELLA, Antonio
2011-01-01

Abstract

This study is focused on the active flow control in the internal flow of turbo-jet engines by Dielectric Barrier Discharges Actuators. In particular the application of this techniques has been studied with the aim of improving the aerodynamic behavior of compressor blades by reducing, or even eliminating, flow separation. A numerical electrostatic model has been implemented in the CFD code, to investigate the aerodynamic behaviour of a transonic compressor rotor with and without plasma actuators.
2011
9781618391803
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11587/361842
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