Active Sensors/Actuators-Based Flow and Noise Control for Aerospace Applications
Abstract
The present work introduces a method for flow and noise control using plasma actuation. The Single Dielectric Barrier Discharge Plasma Actuator (SDBDPA) device is object of study. A discussion of potential applications in flow and noise control in aerospace field is initially done. Then experimental results on separation control applications are presented. The investigated, SDBDPA was manufactured by means of photolithographic technique. Particular attention was paid in materials selection because of possible degradation in plasma environment. The device separation control authority was investigated locating it on a curved plate with a shape designed to reproduce the suction surface of a low pressure turbine (LPT) rotor blade. The changes in the device performances with aging were quantified by monitoring in time the actuator power consumption. Scanning electron microscope (SEM) images on the new and used device were also used to complement the investigation.
Autore Pugliese
Tutti gli autori
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DE GIORGI M.G. Pescini E. , Suma A. , Signore M.A. , Francioso L. , De Pascali C. , A.Ficarella
Titolo volume/Rivista
LECTURE NOTES IN ELECTRICAL ENGINEERING
Anno di pubblicazione
2018
ISSN
1876-1100
ISBN
Non Disponibile
Numero di citazioni Wos
Nessuna citazione
Ultimo Aggiornamento Citazioni
Non Disponibile
Numero di citazioni Scopus
Non Disponibile
0
Ultimo Aggiornamento Citazioni
26/04/2018
Settori ERC
Non Disponibile
Codici ASJC
Non Disponibile
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