Dissipated power and induced velocity fields data of a micro single dielectric barrier discharge plasma actuator for active flow control.

E Pescini,D S Martínez,A Ficarella,L Francioso,M G De Giorgi

doi:10.1016/j.dib.2015.08.011

Abstract

In recent years, single dielectric barrier discharge (SDBD) plasma actuators have gained great interest among all the active flow control devices typically employed in aerospace and turbomachinery applications [1,2]. Compared with the macro SDBDs, the micro single dielectric barrier discharge (MSDBD) actuators showed a higher efficiency in conversion of input electrical power to delivered mechanical power [3,4]. This article provides data regarding the performances of a MSDBD plasma actuator [5,6]. The power dissipation values [5] and the experimental and numerical induced velocity fields [6] are provided. The present data support and enrich the research article entitled “Optimization of micro single dielectric barrier discharge plasma actuator models based on experimental velocity and body force fields” by Pescini et al. [6].

Highlights

Dissipated power and induced velocity fields data of a micro single dielectric barrier discharge plasma actuator for active flow control$
Single dielectric barrier discharge (SDBD) plasma actuators have gained great interest among all the active flow control devices typically employed in aerospace and turbomachinery applications [1,2]
Compared with the macro SDBDs, the micro single dielectric barrier discharge (MSDBD) actuators showed a higher efficiency in conversion of input electrical power to delivered mechanical power [3,4]

Summary

Data Article

Dissipated power and induced velocity fields data of a micro single dielectric barrier discharge plasma actuator for active flow control$. The present data support and enrich the research article entitled “Optimization of micro single dielectric barrier discharge plasma actuator models based on experimental velocity and body force fields” by Pescini et al [6]. Optimization of micro single dielectric barrier discharge plasma actuator models based on experimental velocity and body force fields, Acta Astronaut., 2015, ISSN:0094–5765, http://dx. The data provided here are suitable for comparing the developed micro actuator with others characterized by different geometry and/or constructive materials They can be employed for validations of other CFD codes, which aim to predict the plasma actuation effect on the flow

Type of data

Data format

Value of the data

Findings

Pel ðWÞ