Tuning the Deformation of Flapping Wing to Improve the Flight Efficiency of Dove FWMAV-Reference-Cited by-同舟云学术

Tuning the Deformation of Flapping Wing to Improve the Flight Efficiency of Dove FWMAV

Published:2021-11 Issue:6 Volume:34 Page:04021069
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Xue Dong¹^ORCID,Song Bifeng²

Affiliation:

1. Associate Professor, Northwestern Polytechnical Univ., 127 West Youyi Rd., Beilin District, Xi’an Shaanxi 710072, PR China (corresponding author). ORCID: .

2. Professor, Northwestern Polytechnical Univ., 127 West Youyi Rd., Beilin District, Xi’an Shaanxi 710072, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001320

Reference22 articles.

1. Hovering efficiency comparison of rotary and flapping flight for rigid rectangular wings via dimensionless multi-objective optimization

2. Flexural stiffness in insect wings II. Spatial distribution and dynamic wing bending

3. Wing Rotation and the Aerodynamic Basis of Insect Flight

4. Iterative learning control for a flapping wing micro aerial vehicle under distributed disturbances;He W.;IEEE Trans. Cybern.,2018

5. Flexible Flapping Airfoil Propulsion at Zero Freestream Velocity

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