A Novel Unsteady Vortex Ring Method for Aerodynamic Calculations of a Flapping Wing Rotor-Reference-Cited by-同舟云学术

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A Novel Unsteady Vortex Ring Method for Aerodynamic Calculations of a Flapping Wing Rotor

Published:2024-03 Issue:2 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Xu Huachen¹,Chen Si²^ORCID,Guo Shijun³,Xie Ye⁴,Hu Jie⁵

Affiliation:

1. Master, College of Mechanical and Electrical Engineering, WenZhou Univ., Wenzhou 325035, China.

2. College of Mechanical and Electrical Engineering, Wenzhou Univ., Wenzhou 325035, China (corresponding author). ORCID: .

3. Professor, School of Aerospace, Transport and Manufacturing, Cranfield Univ., Cranfield MK43 0AL, UK.

4. Intelligent Robot Research Centre, Zhejiang Lab, Hangzhou 311121, China.

5. College of Engineering, Jiangxi Agricultural Univ., Nanchang 330045, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5213

Reference26 articles.

1. Forewings match the formation of leading-edge vortices and dominate aerodynamic force production in revolving insect wings

2. Unsteady aerodynamic model of flexible flapping wing

3. Aerodynamic performance of a flyable flapping wing rotor with passive pitching angle variation

4. Design and experimental study of a new flapping wing rotor micro aerial vehicle

5. Effect of Rotation Kinematics and Angle of Attack on Flapping Flight

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