A numerical method was presented for transient heat transfer processes in honeycomb sandwich panels used in metallic thermal protection systems (TPS) under aerodynamic heating.
提出一种计算非稳态气动加热下金属蜂窝板内辐射导热耦合换热数值计算方法。
Knowledge of the thermal performance of Ni-based honeycomb sandwich panels in a thermal protection structure (TPS) is a prerequisite for the design of metal thermal protection structures(MTPS).
掌握热防护系统（TPS）中热结构超合金蜂窝面板在热环境下的传热隔热特性，是飞行器防热结构设计的先决条件。
Impact damage affected tensile ability of honeycomb core sandwich panels seriously.
冲击损伤严重影响了蜂窝夹芯板的抗拉能力。
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