Pescini E, Martínez D S, De Giorgi M G, Francioso L, Ficarella A
University of Salento, Department of Engineering for Innovation, Via per Monteroni, 73100 Lecce, Italy.
Universidad Politécnica de Cartagena, Dep. Ingeníeria Térmica y de Fluidos, c/Dr. Fleming s/n, 30202 Cartagena, Murcia, Spain.
Data Brief. 2015 Aug 28;5:65-70. doi: 10.1016/j.dib.2015.08.011. eCollection 2015 Dec.
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].
近年来，单介质阻挡放电（SDBD）等离子体致动器在航空航天和涡轮机械应用中常用的所有主动流动控制装置中引起了极大的关注[1,2]。与宏观SDBD相比，微单介质阻挡放电（MSDBD）致动器在将输入电功率转换为输出机械功率方面表现出更高的效率[3,4]。本文提供了关于MSDBD等离子体致动器性能的数据[5,6]。给出了功耗值[5]以及实验和数值模拟得到的诱导速度场[6]。目前的数据支持并丰富了Pescini等人发表的题为《基于实验速度和体力场的微单介质阻挡放电等离子体致动器模型优化》的研究文章[6]。
