Aerodynamic optimization design of Z-shaped folding UAV

Aerodynamic optimization design of Z-shaped folding UAV

Aiming at the problems of rolling torque and yaw torque of zigzag UAV, a multi-objective optimization method based on hybrid airfoil parameterization was proposed. The optimization model was established by combining the non dominated sorting genetic algorithm (NSGA-Ⅱ) with hybrid airfoil parameteriz...

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Bibliographic Details
Main Authors: Bin MENG, Jinkang ZHANG, Lele XI, Zexia YANG, Ning ZHOU
Format: Article
Language:zho
Published: Hebei University of Science and Technology 2023-10-01
Series:Journal of Hebei University of Science and Technology
Subjects:
fixed wing aircraft; unmanned aerial vehicle; optimization design; genetic algorithm; airfoil parameterization; flow field modeling; aerodynamic performance
Online Access:https://xuebao.hebust.edu.cn/hbkjdx/article/pdf/b202305003

Internet

https://xuebao.hebust.edu.cn/hbkjdx/article/pdf/b202305003

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