Improving wind turbine blade based on multi-objective particle swarm optimization

Y Li, K Wei, W Yang, Q Wang - Renewable Energy, 2020 - Elsevier
This paper studies a new method for optimizing the design of wind turbine blades.
Compared with the existing blade design methods, the proposed method not only considers …

Iterative symbolic regression for learning transport equations

M Ansari, HA Gandhi, DG Foster, AD White - AIChE Journal, 2022 - Wiley Online Library
Computational fluid dynamics (CFD) analysis is widely used in chemical engineering.
Although CFD calculations are accurate, the computational cost associated with complex …

[HTML][HTML] Modeling novel methodologies for unmanned aerial systems–Applications to the UAS-S4 Ehecatl and the UAS-S45 Bálaam

MAJ Kuitche, RM Botez - Chinese Journal of Aeronautics, 2019 - Elsevier
The rising demand for Unmanned Aerial Systems (UASs) to perform tasks in hostile
environments has emphasized the need for their simulation models for the preliminary …

A comprehensive simulation analysis to optimize the performance of spray evaporator on treating concentrated brine

X Liu, L Yu, L Zhao, Z Hua, H Xue - Desalination, 2023 - Elsevier
The freshwater resources deficient has been dominated the world's science and policy
agenda, owing to the population growth, rapid industrialization, and environmental pollution …

[HTML][HTML] 民机标模高升力构型CAE-AVM-HL 设计及验证

钟敏, 华俊, 王浩, 白俊强 - 空气动力学学报, 2022 - html.rhhz.net
气动标模高升力构型可用于起降状态复杂流动机理研究, CFD 软件验证, 低速风洞试验能力建设
及增升系统噪声测试. 民机气动标模高升力构型CAE-AVM-HL 设计过程中采用基于代理模型的 …

[HTML][HTML] CAE-AVM 标模巡航构型的设计和数据库应用

华俊, 钟敏, 郑遂, 王钢林, 王浩, 白俊强 - 空气动力学学报, 2022 - html.rhhz.net
受计算流体力学(CFD) 与风洞数据相关性研究以及新型远程飞机设计能力建设等需求驱动,
巡航马赫数0.85 量级气动标模的研发日益得到重视, 并受益于先进CFD 方法和风洞精细化试验 …

[HTML][HTML] Preliminary study on heat flux measurement data of TT-0 flight test

LU Enwei, ZUO Linxuan, GUO Zheng… - Chinese Journal of …, 2021 - Elsevier
With the explosive development of aerospace science, the design of the new generation
airliner at higher speeds is attracting more attentions. To achieve this goal, it is necessary to …

[HTML][HTML] CAE-AVM 模型巡航构型风洞试验

王浩, 华俊, 钟敏 - 空气动力学学报, 2022 - html.rhhz.net
基于先进民机对更高巡航马赫数和更高气动效率的需求, 研发了CAE-AVM 模型.
模型的设计巡航马赫数为0.85, 巡航升力系数为0.5, 展弦比为9.0. 2013 年和2018 …

Large Deflection Model and Optimal Design for a Morphing Wing Leading-Edge Skin

F Yang, H Xiao, G Yang, H Guo, R Liu, Z Deng - Journal of Aircraft, 2024 - arc.aiaa.org
Morphing leading edge has great potential to enhance the flight efficiency of a vehicle due to
its smooth and seamless surface. To improve the computational efficiency of leading-edge …

Design and Validation of the Trailing Edge of a Variable Camber Wing Based on a Two-Dimensional Airfoil

J Zhou, X Sun, Q Sun, J Xue, K Song, Y Li, L Dong - Biomimetics, 2024 - mdpi.com
Variable camber wing technology stands out as the most promising morphing technology
currently available in green aviation. Despite the ongoing advancements in smart materials …