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基于图卷积的三维气动外形伴随优化设计

赵典 向锦鹏 宋述芳

空气动力学学报2026,Vol.44Issue(5):160-176,17.
空气动力学学报2026,Vol.44Issue(5):160-176,17.DOI:10.7638/kqdlxxb-2025.0076

基于图卷积的三维气动外形伴随优化设计

GCN-based 3D aerodynamic optimization design based on discrete adjoint method

赵典 1向锦鹏 1宋述芳2

作者信息

  • 1. 西北工业大学 航空学院,西安 710072
  • 2. 西北工业大学 航空学院,西安 710072||飞行器基础布局全国重点实验室,西安 710072
  • 折叠

摘要

Abstract

Gradient-based optimization algorithms,particularly the discrete adjoint method,are widely used in aerodynamic shape optimization due to their independence from design variable dimensionality.However,solving the adjoint equations incurs a computational cost comparable to that of flow field solutions,making it crucial to reduce this burden.In this paper,a three-dimensional aerodynamic shape optimization framework integrating the discrete adjoint method with a graph convolutional neural network(GCN)was proposed.A database of flow fields and optimization gradients for various wings was constructed,and a GCN-based gradient prediction model was developed to replace the traditional discrete adjoint solution.Benefiting from the model's strong capability in topological aggregation and spatial feature extraction,its prediction accuracy reaches approximately 10-5.The proposed framework was applied to the aerodynamic shape optimization of the ONERA M6 wing under aerodynamic and geometric constraints.Compared with the traditional discrete adjoint method,the GCN-based framework reduces computational time by about 76.2%,significantly improving optimization efficiency.This method provides a new technical pathway for efficient and accurate aerodynamic shape optimization.

关键词

梯度优化算法/离散伴随方法/图卷积神经网络/气动外形优化/计算效率

Key words

gradient-based optimization/discrete adjoint method/graph convolutional neural network/aerodynamic shape optimization/computational efficiency

分类

航空航天

引用本文复制引用

赵典,向锦鹏,宋述芳..基于图卷积的三维气动外形伴随优化设计[J].空气动力学学报,2026,44(5):160-176,17.

基金项目

国家自然科学基金(12272316) (12272316)

国家重点研发计划(2023YFB3002800) (2023YFB3002800)

空气动力学学报

0258-1825

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