Optimization of Dielectric Barrier Discharge Plasma Actuators for Icing Control-Reference-Cited by-同舟云学术

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Optimization of Dielectric Barrier Discharge Plasma Actuators for Icing Control

Published:2020-03 Issue:2 Volume:57 Page:383-387
ISSN:1533-3868
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Hu Haiyang¹,Meng Xuanshi¹,Cai Jinsheng¹,Zhou Wenwu²,Liu Yang³,Hu Hui⁴

Affiliation:

1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

2. Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China

3. East Carolina University, Greenville, North Carolina 27858

4. Iowa State University, Ames, Iowa 50011

Funder

National Natural Science Foundation of China

the Aeronautical Science Foundation of China

the National Key Laboratory Research Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference33 articles.

1. Airfoil aerodynamics in icing conditions

2. Aircraft anti-icing and de-icing techniques and modeling

3. Aircraft Characterization in Icing Using Flight Test Data

4. High-Speed Imaging to Quantify Transient Ice Accretion Process over an Airfoil

5. Aerodynamic technologies to improve aircraft performance

Cited by 30 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Periodic Vortices Created by Plasma Actuator with Low Frequency;AIAA Journal;2024-09

2. Recent advancements in flow control using plasma actuators and plasma vortex generators;Heat Transfer;2024-07-24

3. Optimizing electrode arrangement in plasma actuators: a study on induced velocity and efficiency;Fluid Dynamics Research;2024-05-03

4. Virtual leading-edge aero-shaping of an airfoil using a dielectric barrier discharge plasma actuator;Physics of Fluids;2024-05-01

5. Electromechanical ice protection system: de-icing capability prediction considering impedance matching effect;The Aeronautical Journal;2024-03-01

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