Impact of geometric forms on the effectiveness and physical features of POD-based geometric parameterization

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2025-02-01 Epub Date: 2024-11-27 DOI:10.1016/j.ast.2024.109776
Chenliang Zhang , Hongbo Chen , Xiaoyu Xu , Yanhui Duan , Guangxue Wang
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Abstract

Effective geometric parameterization is crucial in aerodynamic shape optimization for enabling flexible surface deformation while maximizing design space coverage. This paper studies the impact of different geometric forms (closed and open curves) on the effectiveness of Proper Orthogonal Decomposition (POD) geometric parameterization and explores the information of physical features contained in the POD bases. The efficiency and design space coverage which are the main indicators of effectiveness. These indicators of two POD-based parameterization methods are tested on a hybrid database and four typical airfoils. The convergence of aerodynamic properties is also investigated in typical airfoils. In addition, a modified application criterion for POD bases is established by the recursive feature elimination method. A feature importance-based explainable AI (xAI) method is also developed, combining Shapley additive explanations (SHAP) and modified application criterion to explore the physical information contained in POD bases. The results indicate that the POD-based parameterization method constructed from open curves can reconstruct database with better efficiency and design space coverage. Additionally, compared to geometric errors, more POD bases may be required to cover the airfoil design space in order to achieve superior aerodynamic accuracy. Significant differences exist in the importance and correlation of POD bases derived from different geometric forms, with those from closed curves providing better reconstruction efficiency for geometric parameters.
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几何形式对基于pod的几何参数化的有效性和物理特征的影响
有效的几何参数化在气动形状优化中至关重要,以实现柔性表面变形,同时最大化设计空间覆盖。本文研究了不同几何形式(闭曲线和开曲线)对适当正交分解几何参数化有效性的影响,探讨了适当正交分解基中包含的物理特征信息。效率和设计空间覆盖率是衡量有效性的主要指标。在混合数据库和四种典型翼型上对两种基于pod的参数化方法的这些指标进行了测试。对典型翼型的气动性能收敛进行了研究。此外,采用递归特征消去法建立了改进的POD基应用准则。提出了一种基于特征重要性的可解释人工智能(xAI)方法,将Shapley加性解释(SHAP)与修正的应用准则相结合,探索POD碱基所包含的物理信息。结果表明,利用开放曲线构造的基于pod的参数化方法重构数据库具有较高的效率和设计空间覆盖率。此外,与几何误差相比,更多的POD基地可能需要覆盖翼型设计空间,以实现优越的空气动力学精度。不同几何形式得到的POD碱基的重要性和相关性存在显著差异,封闭曲线得到的POD碱基对几何参数的重构效率更高。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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