A Computational and Experimental Studies of Flexible Wing Aerodynamics-Reference-Cited by-同舟云学术

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A Computational and Experimental Studies of Flexible Wing Aerodynamics

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Aono Hikaru¹,Chimakurthi Satish Kumar¹,Wu Pin²,Sallstrom Erik²,Stanford Bret²,Cesnik Carlos¹,Ifju Peter²,Ukeiley Lawrence²,Shyy Wei¹

Affiliation:

1. University of Michigan

2. University of Florida

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-554

Reference47 articles.

1. Aerodynamics of Low Reynolds Number Flyers

2. Challenges Facing Future Micro-Air-Vehicle Development

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1. Resonance mechanism of flapping wing based on fluid structure interaction simulation;Chinese Journal of Aeronautics;2024-05

2. Coupled Aeroelastic Study of a Flexible Micro Air Vehicle-Scale Flapping Wing in Hovering Flight;Journal of Aircraft;2022-01

3. Structural Design and Aerodynamic Characteristics of Two Types of Fold-Able Flapping-Wings;Intelligent Robotics and Applications;2022

4. Numerical Simulation Framework for Fluid–Structure Interaction of Flapping Flight;AIAA Journal;2021-09

5. A review on applications of rotary-wing unmanned aerial vehicle charging stations;International Journal of Advanced Robotic Systems;2021-05-01

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