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融合多源数据的防热多孔材料渗透率预测方法OA

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

中文摘要英文摘要

烧蚀热防护是高超声速飞行器重要的热防护手段,热解炭化防热多孔材料是一种烧蚀性热防护材料,其渗透率对输运特性有着显著影响.针对防热多孔材料渗透率公式中经验系数难以获取的问题,构建了包含材料微观结构图像、宏观结构特征参数(最大流与分形维数)的多源异构数据集,采用直接蒙特卡洛模拟粒子类方法计算微结构渗透率,并在此基础上提出了3种基于多源异构数据融合策略的渗透率预测方法:基于决策层的融合策略、基于特征直接拼接的融合策略和基于跨模态注意力机制的融合策略.比较3种不同融合策略的模型预测性能,由于基于跨模态注意力机制的融合策略能够捕捉图像卷积特征与结构特征参数之间的关系,动态调整图像卷积特征与结构特征参数之间的权值,其模型预测效果最优,在预测集上决定系数为0.949 7,平均绝对百分比误差为5.29%,且与单源数据驱动的渗透率预测模型相比,决定系数提高了6%,平均绝对百分比误差下降了41%,能够高效准确地对渗透率进行预测,为实际高超声速飞行器热防护结构精细化设计提供技术支持.

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.

辛炜华;田宇豪;张起鸣;郭京辉;林贵平

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 航空科学与工程学院,北京 100191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 国际创新研究院,杭州 311115

航空航天

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

thermal protective porous materialsmulti-source heterogeneous data fusionpermeabilitydeep learningmulti-scale characterization

《航空学报》 2026 (12)

328-348,21

国家自然科学基金(12572380)中央高校基本科研业务费专项资金(501XYGG2025105029) National Natural Science Foundation of China(12572380)the Fundamental Research Funds for the Central Universities(501XYGG2025105029)

10.7527/S1000-6893.2025.32866

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