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Improved data-driven surrogate models by incorporating variable sensitivity for aerodynamic data modeling

  • Chenzhou Xu
  • , Yunjie Yang
  • , Minchi Kuang
  • , Xing Zhuang
  • , Hongjiang Guo
  • , Zhonghua Han
  • , Ligan Jia
  • , Jihong Zhu
  • Tsinghua University
  • State Key Laboratory of Precision Space-time Information Sensing Technology
  • Jiangsu University of Science and Technology
  • Northwestern Polytechnical University Xian
  • Xinjiang University

Research output: Contribution to journalArticlepeer-review

3 Scopus citations

Abstract

Data-driven surrogate models have become increasingly important in aerospace engineering for the rapid prediction of aerodynamic characteristics. However, when modelling aerodynamic data with varying flight conditions and complex shape parameters, traditional surrogates–such as kriging and fully connected neural network (FCNN)–face major challenges, including high dimensionality, large variable disparities, and limited data availability. Specifically, kriging models suffer from inefficient training processes, while FCNN models struggle with diminished prediction accuracy when confronted with diverse input sets. To address these challenges, this paper introduces two improved surrogate models by incorporating variable sensitivity into the kriging and FCNN models. They employ the analysis of variance to identify the global sensitivity of input variables and utilise K-means clustering to group variables based on their sensitivities. For the kriging model, auxiliary parameters corresponding to the number of clusters are introduced to replace hyperparameters, accelerating model training while maintaining high accuracy. For the FCNN model, input variables are grouped based on their sensitivities, with specialised expert networks handling each group, and a gating network combining their outputs to improve prediction accuracy. The effectiveness of these methods is demonstrated through numerical function examples and two aerodynamic data modelling scenarios: the FDL-5A hypersonic vehicle and the Saenger aerospace plane carrier wing. Results indicate that the proposed approaches significantly enhance the kriging model’s training efficiency, achieving a 98% reduction in hyperparameter tuning time compared to conventional method, with minimal sacrifice in accuracy. Simultaneously, the modifications to the FCNN model not only improve its prediction accuracy but also increase its overall practical utility in engineering applications.

Original languageEnglish
Article number2564830
JournalEngineering Applications of Computational Fluid Mechanics
Volume19
Issue number1
DOIs
StatePublished - 2025

Keywords

  • Aerodynamic data modelling
  • data-driven surrogate model
  • fully connected neural network
  • kriging
  • variable sensitivity

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