What is it about?
A novel anti-icing approach using the surface dielectric barrier discharge plasma actuator driven by high alternative current voltage (AC-SDBD) was developed recently. The configuration of the multi-SDBD actuators is optimized for anti-icing over NACA 0012 airfoil model and tested in the icing wind tunnel.
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This page is a summary of: Optimization of Dielectric Barrier Discharge Plasma Actuators for Icing Control, Journal of Aircraft, March 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035697.
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