Flow field generated by a dielectric barrier discharge plasma actuator in quiescent air at initiation stage-Reference-Cited by-同舟云学术

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Flow field generated by a dielectric barrier discharge plasma actuator in quiescent air at initiation stage

Published:2021-03 Issue:3 Volume:34 Page:13-24
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHANG Xin,CUI Y.D.,TAY Chien Ming Jonathan,KHOO B.C.

Funder

China Aerodynamics Research and Development Center

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference64 articles.

1. An experimental study of icing control using DBD plasma actuator;Cai;Exp Fluids,2017

2. Mechanism study of coupled aerodynamic and thermal effects using plasma actuation for anti-icing;Meng;Phys Fluids,2019

3. Performance and mechanism analysis of nanosecond pulsed surface dielectric barrier discharge based plasma deicer;Wei;Phys Fluids,2019

4. Nanosecond-pulsed dielectric barrier discharge-based plasma-assisted anti-icing: modeling and mechanism analysis;Zhu;J Phys D Appl Phys,2020

5. An experimental study on the thermal effects of duty-cycled plasma actuation pertinent to aircraft icing mitigation;Liu;Int J Heat Mass Tran,2019

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

3. Plasma Actuator Separation Control Investigated with Spectral Proper Orthogonal Decomposition;AIAA Journal;2024-05

4. Design and Development of Power Sources for Plasma Actuators;AIAA SCITECH 2024 Forum;2024-01-04

5. Characteristics of a nanosecond pulsed sliding discharge plasma actuator at low pressure;AIP Advances;2023-07-01

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