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A generative adversarial network based method for aerodynamic configuration design of general aviation aircraft

投稿的翻译标题: 基于生成对抗网络的通航飞行器气动布局设计方法
  • Northwestern Polytechnical University Xian
  • National Key Laboratory of Aircraft Configuration Design

科研成果: 期刊稿件文章同行评审

1 引用 (Scopus)

摘要

Mainstream aerodynamic optimization approaches typically commence with the refinement of initial design stages, concentrating on local optimization within predefined configurations, rather than exploring the diversity of aerodynamic layout alternatives during the conceptual design phase. Recently, generative artificial intelligence has offered a novel solution paradigm for aircraft configuration design. This study presents a generative aerodynamic configuration design methodology based on Generative Adversarial Network(GAN), with application to a small general aviation aircraft. First, the GAN and its variants are evaluated for their capability in representing parametric space and generating aerodynamic configurations. Based on this analysis, a Conditional Wasserstein GAN with Gradient Penalty(CWGAN-GP)is established for efficient generation of aerodynamic configurations. Second, for wing design under low-speed cruise conditions(Mach number 0.2, angle of attack of 2°), the representation capability of different generative models in the parameter space and their ability to generate configurations under given conditions are analyzed, demonstrating the advantages of CWGAN-GP in generative design. Finally, for the conceptual aerodynamic configuration design of a general aviation aircraft under typical cruise conditions (Mach number 0. 6, angle of attack of 2°), the CWGAN-GP model successfully generates a variety of aerodynamic configurations using the lift coefficient and lift-to-drag ratio as conditional parameters. By extending beyond the training parameter ranges, the proposed method exhibits strong generalization and extrapolation capabilities, capable of producing different aerodynamic shapes outside the original condition space. These results indicate that the generative design methodology presented offers a promising new paradigm for next-generation aircraft aerodynamic configuration exploration and innovation.

投稿的翻译标题基于生成对抗网络的通航飞行器气动布局设计方法
源语言英语
期刊论文编号132518
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
47
6
DOI
出版状态已出版 - 25 3月 2026

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