Computational Investigation of a Doubly Hinged Flapping-Wing Model-Reference-Cited by-同舟云学术

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Computational Investigation of a Doubly Hinged Flapping-Wing Model

Published:2012-12 Issue:12 Volume:50 Page:2643-2654
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zhang Yunfei¹,Ye Zhengyin¹,Xie Fei²

Affiliation:

1. National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China

2. Sichuan Academy of Aerospace Technology, 610100 Chengdu, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J051108

Reference38 articles.

1. Recent progress in flapping wing aerodynamics and aeroelasticity

2. Series A: Mathematical, Physical and Engineering Sciences;Liu P.

3. Numerical Simulation of a Flapping Foil with Chordwise or Spanwise Flexibility

4. Effect of spanwise flexibility on flapping wing propulsion

5. Computational Aeroelasticity Framework for Analyzing Flapping Wing Micro Air Vehicles

Cited by 1 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. A Computational Study of Wall Effects on the Aeroelastic Behavior of Spanwise Flexible Wings;International Journal of Aeronautical and Space Sciences;2019-04-30

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