The niching-based adaptive space reconstruction method for airfoil aerodynamic/stealth design

Wei Zhang, Zhenghong Gao, Chao Wang, Lu Xia

科研成果: 期刊稿件文章同行评审

4 引用 (Scopus)

摘要

The airfoils for flying wing aircraft need good aerodynamic, trim and stealth performance, and these unconventional requirements would lead to multimodality in airfoil design optimizations. It would be time-consuming for a single-point sequence sampling method, like the Efficient Global Optimization method (EGO), to obtain the global optima over the entire design space, and the traditional multi-start sampling approach would tend to find the local minima which were well-explored by the surrogate model. Thus, the Niching-based Adaptive Space Reconstruction method (NASR) was introduced to enhance the performance of the EGO for aerodynamic/stealth optimizations in this paper. The proposed method adopted a Niching-based multiple points sampling method to simultaneously search out the locations of multiple local minima of the EI function, which did not rely on the starting points and avoided converging to the same local minima. Moreover, it would check the neighborhood of the local minima and focus on the local minima which were not well-explored to decrease computational cost. To decrease the risk of missing promising regions, different expansion strategies were applied to adjust the size of design intervals in different iterations. Several numerical and structural optimization problems were studied to test and verify the efficiency and robustness of NASR. Then, airfoil optimizations considering aerodynamic, stealth and aero/stealth performance by NASR were conducted. It was shown that the aerodynamic performance of the aerodynamic optimized result was comparable with the aero/stealth optimization, and the stealth performance of the stealth optimized result was better than the aero/stealth optimization. The conflictions between Radar Cross Sections (RCS) reduction and drag reduction were not very prominent. Moreover, although the pitch positive moment constraint would damage the lift-drag characteristics, it could be beneficial to RCS reduction based on the current study.

源语言英语
文章编号159
期刊Structural and Multidisciplinary Optimization
66
7
DOI
出版状态已出版 - 7月 2023

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