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基于目标检验条件生成对抗网络的翼型反设计方法

孟宪超 陶俊

航空学报2025,Vol.46Issue(10):120-134,15.
航空学报2025,Vol.46Issue(10):120-134,15.DOI:10.7527/S1000-6893.2024.31182

基于目标检验条件生成对抗网络的翼型反设计方法

An airfoil inverse design method based on target testing conditional generative adversarial network

孟宪超 1陶俊1

作者信息

  • 1. 复旦大学 航空航天系,上海 200433
  • 折叠

摘要

Abstract

A Target Testing Conditional Generative Adversarial Network(TT-CGAN)is developed and applied to air-foil inverse design.This network extends the Conditional Generative Adversarial Network(CGAN)by integrating a Multi-Layer Perceptron(MLP)tester,so as to enhance the capability of CGAN in evaluating the impact of additional conditions on target testing.Utilizing the UIUC airfoil database,797 real airfoils were selected,and their correspond-ing aerodynamic parameters were calculated by solving the Reynolds-Averaged Navier-Stokes(RANS)equations to construct a comprehensive airfoil database.The airfoil shapes were parameterized using the Class Shape Transforma-tion(CST)method,transforming the geometric parameters from 100 to 14 CST parameters.Multi-modal aerody-namic parameters,including lift coefficient,drag coefficient,and surface pressure distribution,were fused using the feature-level fusion approach.These parameters were compared with the aerodynamic parameters based solely on lift and drag coefficients,which served as auxiliary conditions for the network during the airfoil inverse design process.The results indicate that the TT-CGAN based inverse design method generates more accurate airfoils,with an average root mean square error of 1.779×10-3 and an average mean absolute error of 1.351×10-3 in airfoil geometry.The generated airfoils were further validated through numerical simulations by solving the RANS equations,demonstrating an average relative error of 3.599 8%for the lift coefficient and 3.723 9%for the drag coefficient,confirming that the generated airfoils can meet the specified design criteria.Analysis of the lift-to-drag ratio distributions reveals that 40%of the test airfoils achieved lift-to-drag ratios within the[20,30)range,compared to only 16%in the training set.This finding highlights the method's capability to make accurate predictions even within data-sparse regions,showcasing its generalizability.

关键词

翼型反设计/条件生成对抗网络(CGAN)/多模态数据融合/类别/形状函数变换/参数化

Key words

airfoil inverse design/conditional generative adversarial network(CGAN)/multi-modal data fusion/class shape transformation(CST)/parameterization

分类

航空航天

引用本文复制引用

孟宪超,陶俊..基于目标检验条件生成对抗网络的翼型反设计方法[J].航空学报,2025,46(10):120-134,15.

航空学报

OA北大核心

1000-6893

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