Knowledge Transfer-Accelerated Intelligent Aerodynamic Design Optimization

被引:1
|
作者
Guo Z. [1 ]
Li C. [1 ]
Song L. [1 ]
Li J. [1 ]
Feng Z. [1 ]
机构
[1] School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an
关键词
aerodynamic shape optimization; Bayesian optimization; knowledge transfer; multi-fidelity surrogate model; variational autoencoder;
D O I
10.7652/xjtuxb202310006
中图分类号
学科分类号
摘要
To address the gap between the minimum number of evaluations required for refined aerodynamic shape optimization tasks and the maximum number of evaluations constrained by the mission period, a study on intelligent aerodynamic design optimization accelerated by knowledge transfer was conducted based on the concept of transfer learning in the field of machine learning. Firstly, an airfoil variational autoencoder(VAE)model was built. The model's decoder enabled the intelligent parameterization of aerodynamic shapes, while its encoder unified samples from source tasks into the parameterization space of the target task. Secondly, the Bayesian transfer optimization algorithm was established, incorporating both single and multi-fidelity surrogate models. Then, an intelligent transfer optimization framework for aerodynamic shapes was established by integrating the airfoil VAE model and Bayesian transfer optimization algorithm. Last, task correlation analysis was made to discuss the mechanism of the optimization process accelerated by knowledge transfer. The results from airfoil optimization test demonstrate that such a framework improves the performance of median of the optimal solution by 4.8% compared to using VAE optimization lack of knowledge transfer, and by more than 19.9% compared to other methods, confirming the effectiveness of knowledge transfer strategy. © 2023 Xi'an Jiaotong University. All rights reserved.
引用
收藏
页码:53 / 63
页数:10
相关论文
共 31 条
  • [1] LI Jichao, ZHANG Mengqi, MARTINS J R R A, Et al., Efficient aerodynamic shape optimization with deep-learning-based geometric filtering, AIAA Journal, 58, 10, pp. 4243-4259, (2020)
  • [2] XI Guang, WANG Zhiheng, WANG Shangjin, Aerodynamic optimization design of turbomachinery with approximation model method, Journal of Xi'an Jiaotong University, 41, 2, pp. 125-135, (2007)
  • [3] HUANG Song, YANG Chengwu, HAN Ge, Et al., Optimal design of a controlled diffusion airfoil with the whale algorithm, Journal of Xi'an Jiaotong University, 54, 3, pp. 49-57, (2020)
  • [4] WANG Qineng, SONG Liming, GUO Zhendong, Et al., Study on turbomachinery optimization based on dynamic interaction analysis [J/OL], Journal of Xi'an Jiaotong University, 2023, 7, pp. 1-10
  • [5] GUO Zhendong, SONG Liming, LI Jun, Et al., Meta model-based global design optimization and exploration method, Journal of Propulsion Technology, 36, 2, pp. 207-216, (2015)
  • [6] SHAN Songqing, WANG G G., Survey of modeling and optimization strategies to solve high-dimensional design problems with computationally-expensive black-box functions, Structural and Multidisciplinary Optimization, 41, 2, pp. 219-241, (2010)
  • [7] MASTERS D A, TAYLOR N J, RENDALL T C S, Et al., Geometric comparison of aerofoil shape parameterization methods, AIAA Journal, 55, 5, pp. 1575-1589, (2017)
  • [8] CHEN Wei, CHIU K, FUGE M D., Airfoil design parameterization and optimization using Bézier generative adversarial networks, AIAA Journal, 58, 11, pp. 4723-4735, (2020)
  • [9] WANG Yuyang, SHIMADA K, FARIMANI A B., Airfoil GAN: encoding and synthesizing airfoils for aerodynamic shape optimization, Journal of Computational Design and Engineering, (2023)
  • [10] VIANA F A C, SIMPSON T W, BALABANOV V, Et al., Special section on multidisciplinary design optimization: metamodeling in multidisciplinary design optimization: how far have we really come, AIAA Journal, 52, 4, pp. 670-690, (2014)