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融合多源数据的防热多孔材料渗透率预测方法

辛炜华 田宇豪 张起鸣 郭京辉 林贵平

航空学报2026,Vol.47Issue(12):328-348,21.
航空学报2026,Vol.47Issue(12):328-348,21.DOI:10.7527/S1000-6893.2025.32866

融合多源数据的防热多孔材料渗透率预测方法

Permeability prediction method for thermal protective porous materials by integrating multi-source data

辛炜华 1田宇豪 2张起鸣 2郭京辉 2林贵平3

作者信息

  • 1. 北京航空航天大学 航空科学与工程学院,北京 100191||北京航空航天大学 宇航学院,北京 100191
  • 2. 北京航空航天大学 航空科学与工程学院,北京 100191
  • 3. 北京航空航天大学 国际创新研究院,杭州 311115
  • 折叠

摘要

Abstract

Ablative thermal protection is an important thermal protection method for hypersonic vehicles.Porous pyro-lyzed carbon for thermal protection materials are a type of ablative thermal protective material,whose permeability sig-nificantly influences transport characteristics.To address the issue of difficulty in obtaining empirical coefficients in per-meability formulas for thermal protective porous materials,a multi-source heterogeneous dataset is constructed,incor-porating material microstructure images and macroscopic structural characteristic parameters(maximum flow and frac-tal dimension).A particle-based method named direct simulation Monte Carlo is employed to calculate the permeabil-ity of the microstructure.Based on this,three permeability prediction methods using multi-source heterogeneous data fusion strategies are proposed:a decision-level fusion strategy,a fusion strategy based on direct concatenation of multi-source data features,and a fusion strategy based on a cross-modal attention mechanism for multi-source data.By comparing the predictive performance of the three fusion strategies,the strategy based on the cross-modal atten-tion mechanism demonstrates the best performance.This strategy captures the relationship between image convolu-tional features and structural parameters and dynamically adjusts the weights between them.On the test set,the coef-ficient of determination is 0.949 7,and the Mean Absolute Percentage Error is 5.29%.Compared with single-source data-driven permeability prediction models,the coefficient of determination improves by 6%,and the Mean Absolute Percentage Error decreases by 41%.This method enables efficient and accurate prediction of permeability,providing technical support for the refined design of thermal protection structures in actual hypersonic vehicles.

关键词

防热多孔材料/多源异构数据融合/渗透率/深度学习/多尺度表征

Key words

thermal protective porous materials/multi-source heterogeneous data fusion/permeability/deep learning/multi-scale characterization

分类

航空航天

引用本文复制引用

辛炜华,田宇豪,张起鸣,郭京辉,林贵平..融合多源数据的防热多孔材料渗透率预测方法[J].航空学报,2026,47(12):328-348,21.

基金项目

国家自然科学基金(12572380) (12572380)

中央高校基本科研业务费专项资金(501XYGG2025105029) National Natural Science Foundation of China(12572380) (501XYGG2025105029)

the Fundamental Research Funds for the Central Universities(501XYGG2025105029) (501XYGG2025105029)

航空学报

1000-6893

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