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Research on missile aerodynamic data generation technology based on multi-credibility proxy model
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Pengzhen FU1, Jiangtao CHEN2, Peihong ZHANG2
Chinese Journal of Computational Mechanics | 2025, 42(5) : 714 - 721
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Chinese Journal of Computational Mechanics | 2025, 42(5): 714-721
Research Papers
Research on missile aerodynamic data generation technology based on multi-credibility proxy model
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Pengzhen FU1, Jiangtao CHEN2, Peihong ZHANG2
Affiliations
  • 1.School of Computer Science and Technology, Southwest University of Science and Technology, Mianyang 621010, China
  • 2.Computational Aerodynamic Institute of China Aerodynamic Research & Development Center, Mianyang 621000, China
Published: 2025-10-28 doi: 10.7511/jslx20240612002
Outline
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A surrogate model is a new research idea direction of aerodynamic data generation. A traditional surrogate model relies on a large number of high-precision simulation sample points and their responses values to ensure the accuracy of the model. A multi-credibility surrogate model can reduce the computational cost while maintaining a certain accuracy by integrating multi-layer high and low credibility models, which is of great significance for reducing a missile development cycle. In this paper, the influence of different numbers of low-confidence sample points on the multi-confidence model and the optimal ratio of high-low-confidence sample points are studied, and a multi-confidence sampling method suitable for aerodynamics data is proposed. It is applied to the construction of three multi-credibility surrogate models in the prediction of missile aerodynamic data, among which the Co-Kriging model has the best comprehensive prediction effect. The recommended ratio of high and low confidence sample size is between 1: 4 and 1: 3.

erodynamic data  /  multi-trusted proxy model  /  the proportion of high and low confidence sample points  /  K-means clustering algorithm
Pengzhen FU, Jiangtao CHEN, Peihong ZHANG. Research on missile aerodynamic data generation technology based on multi-credibility proxy model[J]. Chinese Journal of Computational Mechanics, 2025 , 42 (5) : 714 -721 . DOI: 10.7511/jslx20240612002
Year 2025 volume 42 Issue 5
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Article Info
doi: 10.7511/jslx20240612002
  • Receive Date:2024-06-12
  • Online Date:2026-03-24
  • Published:2025-10-28
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  • Received:2024-06-12
  • Revised:2024-07-29
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    1.School of Computer Science and Technology, Southwest University of Science and Technology, Mianyang 621010, China
    2.Computational Aerodynamic Institute of China Aerodynamic Research & Development Center, Mianyang 621000, China
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Number of
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鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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