Utilization of Thermal Effect Induced by AC-DBD Plasma Generation for Aircraft Icing Mitigation
Author:
Affiliation:
1. Iowa State University
2. Northwestern Polytechnical University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0168
Reference26 articles.
1. Aircraft icing
2. An experimental study on the characteristics of wind-driven surface water film flows by using a multi-transducer ultrasonic pulse-echo technique
3. Iced-airfoil aerodynamics
4. Aircraft anti-icing and de-icing techniques and modeling
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1. A hybrid plasma de-icing actuator by using SiC hydrophobic coating-based quartz glass as barrier dielectric;Journal of Physics D: Applied Physics;2021-07-01
2. Development of an Anti-Icing Computational Fluid Dynamics Code;AIAA Scitech 2020 Forum;2020-01-05
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