Design and experiment of a bionic flapping wing mechanism with flapping–twist–swing motion based on a single rotation-Reference-Cited by-同舟云学术

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Design and experiment of a bionic flapping wing mechanism with flapping–twist–swing motion based on a single rotation

Published:2020-06-01 Issue:6 Volume:10 Page:065018
ISSN:2158-3226
Container-title:AIP Advances
language:en
Short-container-title:AIP Advances

Author:

Ji Bing¹^ORCID,Zhu Qiaolin¹,Guo Shijun²,Yang Fan¹,Li Yushuai¹,Zhu Zenggang¹,Chen Si³,Song Rui¹,Li Yibin¹

Affiliation:

1. School of Control Science and Engineering, Shandong University, Jinan 250061, China

2. School of Aerospace, Transport and Manufacturing, Cranfield University, Cranfield MK43 0AL, United Kingdom

3. College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Link

http://aip.scitation.org/doi/pdf/10.1063/5.0008792

Reference25 articles.

1. T. J. Muller, Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications Progress in Astronautics and Aeronautics (AIAA, 2001), p. 195.

2. Unsteady aerodynamics and flow control for flapping wing flyers

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