Integral Airfoil Generation of Multi-rotor Aircraft Based on Optimization of Upper Wing Contour and CFD Simulation

Integral Airfoil Generation of Multi-rotor Aircraft Based on Optimization of Upper Wing Contour and CFD Simulation

Regarding the airfoil optimization design of multi-rotor unmanned aerial vehicles, this paper proposes an integral airfoil design method based on upper airfoil contour optimization. Firstly, by designing concave descent input curves with 0-1 distribution, the upper arc of different optimized airfoil...

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Bibliographic Details
Main Authors: Z. Wang, Y. Zhu, Q. Yuan, W. B. Gu, X. B. Xie
Format: Article
Language:English
Published: Isfahan University of Technology 2024-02-01
Series:Journal of Applied Fluid Mechanics
Subjects:
airfoil design
parameterization method
upper airfoil contour optimization
computational fluid dynamics
aerodynamic performance
Online Access:https://www.jafmonline.net/article_2410_33e6e01b946f60aa220943aa8d30079b.pdf

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