Mechanism study of coupled aerodynamic and thermal effects using plasma actuation for anti-icing
Author:
Affiliation:
1. Department of Fluid Mechanics, Northwestern Polytechnical University, Xi’an 710072, China
2. Department of Aerospace Engineering, Iowa State University, Ames, Iowa 50011, USA
Funder
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5086884
Reference42 articles.
1. Aircraft icing
2. AIRCRAFT ICING
3. Anti-icing and de-icing techniques for wind turbines: Critical review
4. Mixed ice accretion on aircraft wings
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