Effect of dielectric barrier discharge plasma actuator on the dynamic moment behavior of pitching airfoil at low Reynolds number-Reference-Cited by-同舟云学术

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Effect of dielectric barrier discharge plasma actuator on the dynamic moment behavior of pitching airfoil at low Reynolds number

Published:2021-04 Issue:4 Volume:33 Page:043603
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Huang Guangjing¹,Dai Yuting¹^ORCID,Yang Chao¹,Wu You¹,Xia Yingjie¹

Affiliation:

1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China

Funder

National Natural Science Foundation of China

National Key Research and Development Program of China

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

https://aip.scitation.org/doi/pdf/10.1063/5.0048235

Reference39 articles.

1. Membrane wing aerodynamics for micro air vehicles

2. AERODYNAMICS OF SMALL VEHICLES

3. Low-Reynolds-Number Airfoils

4. Effect of active oscillation of local surface on the performance of low Reynolds number airfoil

5. On the importance of aerodynamic and structural geometrical nonlinearities in aeroelastic behavior of high-aspect-ratio wings

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

2. Stall flutter mitigation of an airfoil by active surface morphing;Physics of Fluids;2024-08-01

3. Aerodynamic characteristics of a pitching airfoil with leading-edge morphing;Chinese Journal of Aeronautics;2024-07

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

5. Flow control by dielectric barrier discharge plasma actuators for a rectangular jet with inlet disturbance;Physics of Fluids;2024-03-01

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