Affiliation:
1. Centre for Mechanical and Aerospace Science and Technologies (C-MAST), University of Beira Interior, 6201-001 Covilhã, Portugal
Abstract
Plasma actuators have demonstrated great potential for active flow control applications, including boundary layer control, flow separation delay, turbulence control, and aircraft noise reduction. In particular, the material used as a dielectric barrier is crucial for the proper operation of the device. Currently, the variety of dielectrics reported in the literature is still quite restricted to polymers including Kapton, Teflon, poly(methyl methacrylate) (PMMA), Cirlex, polyisobutylene (PIB) rubber, or polystyrene. Nevertheless, several studies have highlighted the fragilities of polymeric dielectric layers when actuators operate at significantly high-voltage and -frequency levels or for long periods. In the current study, we propose the use of alumina-based ceramic composites as alternative materials for plasma actuator dielectric layers. The alumina composite samples were fabricated and characterized in terms of microstructure, electrical parameters, and plasma-induced flow velocity and compared with a conventional Kapton-based actuator. It was concluded that alumina-based dielectrics are suitable materials for plasma actuator applications, being able to generate plasma-induced flow velocities of approximately 4.5 m/s. In addition, it was verified that alumina-based ceramic actuators can provide similar fluid mechanical efficiencies to Kapton actuators. Furthermore, the ceramic dielectrics present additional characteristics, such as high-temperature resistance, which are not encompassed by conventional Kapton actuators, which makes them suitable for high-temperature applications such as turbine blade film cooling enhancement and plasma-assisted combustion. The high porosity of the ceramic results in lower plasma-induced flow velocity and lower fluid mechanical efficiency, but by minimizing the porosity, the fluid mechanical efficiency is increased.
Funder
Portuguese Foundation for Science and Technology
contract of João Nunes-Pereira within the framework of the FCT Stimulus of Scientific Employment, Individual Support
Reference53 articles.
1. Clyde Warsop, Active Flow Control Using MEMS (2004, February 01). In MEMS Aerospace Applications, RTO/NATO. Available online: https://apps.dtic.mil/sti/citations/tr/ADA425494.
2. Wang, J., and Feng, L. (2018). Flow Control Techniques and Applications, Cambridge University Press (CUP).
3. Batikh, A., Baldas, L., and Colin, S. (2023, September 20). Application of Active Flow Control on Aircrafts—State of the Art. Available online: https://hal.science/hal-01820331.
4. Effects of AC Dielectric Barrier Discharge Plasma Actuator Location on Flow Separation and Airfoil Performance;Bouremel;Procedia Eng.,2013
5. Viguera, R., Anzai, Y., Sasaki, Y., and Nonomura, T. (2023). Experimental Observations of Transient Flows in Separation Control Using a Plasma Actuator. Actuators, 12.