材料科学
复合数
传热
夹芯板
航天飞机热防护系统
复合材料
热传导
热的
烧蚀
热方程
机械
热力学
热保护
工程类
物理
航空航天工程
量子力学
作者
Shengbo Shi,Yifan Wang,Yan Li,Peijie Sun,Maoyuan Li,Shuo Tang
标识
DOI:10.1016/j.compstruct.2020.112623
摘要
Structurally integrated thermal protection system (ITPS) was investigated, which has both load-carrying and thermal protection capacities. A novel all-composite sandwich panel with corrugated core was fabricated using the hot press molding method. According to the surface ablation and transient heat transfer theory, an approximate analytical model for predicting the coupled ablation and thermal response was presented for the composite sandwich panel. The effects of pyrolysis reactions, phase transitions, evaporation of quartz fibers, generation of decomposition gases, as well as surface ablation were considered in the mathematical model. After the heat conduction equations had been rewritten by separation of variables and further homogenized by a linearized approach, the governing differential equations were solved using Helmholtz formula and orthogonal expansion technique. A thermal exposure experimental test was performed to validate the approximate analytical model. The monitored temperature–time profiles in the thickness direction are in good agreement with the simulated results. The developed all-composite ITPS successfully protects any payload from an exposure to heat fluxes in the 300–500 kW/m2 range during approximately 2 min.
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