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Integrated Aerodynamic and Stealth Design of Wing Airfoil Based on Generative Model

CHI Xinyan ZENG Lifang LI Jun LI Yuhang

Transactions of Nanjing University of Aeronautics and Astronautics2026，Vol.43Issue(3)：P.427-442,16.

Transactions of Nanjing University of Aeronautics and Astronautics2026，Vol.43Issue(3)：P.427-442,16.DOI:10.16356/j.1005-1120.2026.03.008

Integrated Aerodynamic and Stealth Design of Wing Airfoil Based on Generative Model

CHI Xinyan ¹ZENG Lifang ²LI Jun ³LI Yuhang¹

作者信息

1. School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,P.R.China
2. School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,P.R.China Zhejiang Key Laboratory of Intelligent High Speed UAV Technology,Zhejiang University,Hangzhou 310027,P.R.China
3. School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027,P.R.China Huanjiang Laboratory,Zhuji 311800,P.R.China
折叠

摘要

关键词

integrated aerodynamic-stealth design/generative design/diffusion model/class-shape transformation(CST)parameterization/lift-to-drag ratio/radar cross-section(RCS)

分类

航空航天

引用本文复制引用

CHI Xinyan,ZENG Lifang,LI Jun,LI Yuhang..Integrated Aerodynamic and Stealth Design of Wing Airfoil Based on Generative Model[J].Transactions of Nanjing University of Aeronautics and Astronautics,2026,43(3):P.427-442,16.

基金项目

supported by the Fundamental Research Funds for the Central Universities(No.226-2025-00075) （No.226-2025-00075）

the Defense Industrial Technology Development Program(No.JCKY2023205B013) （No.JCKY2023205B013）

the Leading Talent Project for Scientific and Technological Innovation in Zhejiang Province(No.2023R5220). （No.2023R5220）

Transactions of Nanjing University of Aeronautics and Astronautics

ISSN：1005-1120

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