TY - JOUR
T1 - Permeability prediction method for thermal protective porous materials by integrating multi-source data
AU - XIN, Weihua
AU - TIAN, Yuhao
AU - ZHANG, Qiming
AU - GUO, Jinghui
AU - LIN, Guiping
N1 - Publisher Copyright:
© (2026), (Chinese Society of Astronautics). All rights reserved.
PY - 2026
Y1 - 2026
N2 - Ablative thermal protection is an important thermal protection method for hypersonic vehicles. Porous pyrolyzed carbon for thermal protection materials are a type of ablative thermal protective material,whose permeability significantly influences transport characteristics. To address the issue of difficulty in obtaining empirical coefficients in permeability formulas for thermal protective porous materials,a multi-source heterogeneous dataset is constructed,incorporating material microstructure images and macroscopic structural characteristic parameters(maximum flow and fractal dimension). A particle-based method named direct simulation Monte Carlo is employed to calculate the permeability 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 attention mechanism demonstrates the best performance. This strategy captures the relationship between image convolutional features and structural parameters and dynamically adjusts the weights between them. On the test set,the coefficient 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.
AB - Ablative thermal protection is an important thermal protection method for hypersonic vehicles. Porous pyrolyzed carbon for thermal protection materials are a type of ablative thermal protective material,whose permeability significantly influences transport characteristics. To address the issue of difficulty in obtaining empirical coefficients in permeability formulas for thermal protective porous materials,a multi-source heterogeneous dataset is constructed,incorporating material microstructure images and macroscopic structural characteristic parameters(maximum flow and fractal dimension). A particle-based method named direct simulation Monte Carlo is employed to calculate the permeability 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 attention mechanism demonstrates the best performance. This strategy captures the relationship between image convolutional features and structural parameters and dynamically adjusts the weights between them. On the test set,the coefficient 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.
KW - deep learning
KW - multi-scale characterization
KW - multi-source heterogeneous data fusion
KW - permeability
KW - thermal protective porous materials
KW - 多 尺 度 表 征
KW - 多 源 异 构 数 据 融 合
KW - 深 度 学 习
KW - 渗 透 率
KW - 防 热 多 孔 材 料
UR - https://www.scopus.com/pages/publications/105046352870
U2 - 10.7527/S1000-6893.2025.32866
DO - 10.7527/S1000-6893.2025.32866
M3 - 文章
AN - SCOPUS:105046352870
SN - 1000-6893
VL - 47
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 12
M1 - 432866
ER -