Effect of spanwise folding on the aerodynamic performance of three dimensional flapping flat wing-Reference-Cited by-同舟云学术

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Effect of spanwise folding on the aerodynamic performance of three dimensional flapping flat wing

Published:2022-02 Issue:2 Volume:34 Page:021906
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Lang Xinyu¹,Song Bifeng¹²³,Yang Wenqing¹²³,Yang Xiaojun¹²³

Affiliation:

1. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China

2. Research & Development Institute of Northwestern Polytechnical University in Shenzhen, Shenzhen 518057, China

3. Yangtze River Delta Research Institute of Northwestern Polytechnical University, Taicang 215400, China

Funder

National Natural Science Foundation of China

Key R&D Program in Shaanxi Province of China

the foundation of National Key Laboratory of Science and Technology on Aerodynamic Design and Research

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/10.1063/5.0078844

Reference42 articles.

1. Avian Wing Geometry and Kinematics

2. Avian wing geometry and kinematics of a free-flying barn owl in flapping flight

3. Kinematics and aerodynamics of avian upstrokes during slow flight

4. Bending rules for animal propulsion

5. Flapping Wing Flight Can Save Aerodynamic Power Compared to Steady Flight

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1. The Coupled Wing Morphing of Ornithopters Improves Attitude Control and Agile Flight;Machines;2024-07-19

2. Effects of dynamical spanwise retraction and stretch on flapping-wing forward flights;Chinese Journal of Aeronautics;2024-04

3. Effects of symmetry-breaking mechanisms on the flow field around magnetic-responsive material appendages that mimic swimming strokes;Physical Review Fluids;2024-02-13

4. The Effect of Spanwise Folding on the Aerodynamic Performance of a Passively Deformed Flapping Wing;Biomimetics;2024-01-10

5. Calculation and Selection of Airfoil for Flapping-Wing Aircraft Based on Integral Boundary Layer Equations;Aerospace;2023-12-31

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