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翼型盒式机翼布局的气动优化及其机器学习集成方法

哈桑·梅赫迪 邓中敏 雷东内·斯特凡 萨努西·B.穆罕默德

南京航空航天大学学报(英文版)2025,Vol.42Issue(6):789-800,12.
南京航空航天大学学报(英文版)2025,Vol.42Issue(6):789-800,12.DOI:10.16356/j.1005-1120.2025.06.006

翼型盒式机翼布局的气动优化及其机器学习集成方法

Aerodynamic Optimization of Box-Wing Planform Through Machine Learning Integration

哈桑·梅赫迪 1邓中敏 1雷东内·斯特凡 2萨努西·B.穆罕默德3

作者信息

  • 1. 北京航空航天大学杭州创新研究院,杭州 310020,中国
  • 2. 香港科技大学机械与航空航天工程系,香港 999077,中国
  • 3. 哈尔滨工业大学(深圳)机电工程与自动化学院,深圳 518057,中国
  • 折叠

摘要

Abstract

This study discusses a machine learning-driven methodology for optimizing the aerodynamic performance of both conventional,like common research model(CRM),and non-conventional,like Bionica box-wing,aircraft configurations.The approach leverages advanced parameterization techniques,such as class and shape transformation(CST)and Bezier curves,to reduce design complexity while preserving flexibility.Computational fluid dynamics(CFD)simulations are performed to generate a comprehensive dataset,which is used to train an extreme gradient boosting(XGBoost)model for predicting aerodynamic performance.The optimization process,using the non-dominated sorting genetic algorithm(NSGA-Ⅱ),results in a 12.3%reduction in drag for the CRM wing and an 18%improvement in the lift-to-drag ratio for the Bionica box-wing.These findings validate the efficacy of machine learning based method in aerodynamic optimization,demonstrating significant efficiency gains across both configurations.

关键词

气动优化/盒式机翼/机器学习/计算流体力学

Key words

aerodynamic optimization/box-wing/machine learning/computational fluid dynamics(CFD)

分类

信息技术与安全科学

引用本文复制引用

哈桑·梅赫迪,邓中敏,雷东内·斯特凡,萨努西·B.穆罕默德..翼型盒式机翼布局的气动优化及其机器学习集成方法[J].南京航空航天大学学报(英文版),2025,42(6):789-800,12.

基金项目

We would like to extend our sincere gratitude to Azad Khandoker from JKU Linz for his continu-ous support and guidance in research and innovation,which served as a major inspiration for this study.Our heartfelt thanks also go to the Bionica-aircraft team for their valuable resources,insightful feedback,and constructive criticism,which significantly improved the quality of this manuscript. ()

南京航空航天大学学报(英文版)

1005-1120

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