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Coupled ablation and thermal behavior of an all-composite structurally integrated thermal protection system: Fabrication and modeling

机译:全组合结构集成热保护系统的耦合消融和热行为:制造和建模

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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/m(2) range during approximately 2 min.
机译:研究了结构集成的热保护系统(ITPS),其具有负载承载和热保护能力。使用热压模塑方法制造具有波纹芯的新型全组合夹芯板。根据表面消融和瞬态传热理论,提出了一种预测耦合消融和热响应的近似分析模型,用于复合夹层板。在数学模型中考虑了热解反应,阶段转变,蒸发的石英纤维,分解气体的产生以及表面消融的影响。通过分离变量并通过线性化方法进一步均化被重写之后,使用Helmholtz公式和正交的膨胀技术来解决控制微分方程。进行热暴露实验试验以验证近似分析模型。厚度方向上的监测温度时间曲线与模拟结果吻合良好。开发的全综合ITP在大约2分钟内成功地保护任何有效载荷从暴露于300-500 kW / m(2)范围内的热通量。

著录项

  • 来源
    《Composite Structures》 |2020年第11期|112623.1-112623.10|共10页
  • 作者单位

    Northwestern Polytech Univ Sch Astronaut Shaanxi Aerosp Flight Vehicle Design Key Lab Xian 710072 Peoples R China|Univ Bristol Dept Aerosp Engn Bristol Composites Inst ACCIS Bristol BS8 1TR Avon England;

    China Acad Launch Vehicle Technol Sci & Technol Space Phys Lab Beijing 100076 Peoples R China;

    Shanghai Aerosp Syst Res Inst Shanghai 201108 Peoples R China;

    Shanghai Aerosp Syst Res Inst Shanghai 201108 Peoples R China;

    Beijing Inst Mech & Elect Engn Beijing 100038 Peoples R China;

    Northwestern Polytech Univ Sch Astronaut Shaanxi Aerosp Flight Vehicle Design Key Lab Xian 710072 Peoples R China|Univ Bristol Dept Aerosp Engn Bristol Composites Inst ACCIS Bristol BS8 1TR Avon England;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Thermal protection system; Composite sandwich panels; Approximate analytical model; Thermal behavior; Ablation;

    机译:热保护系统;复合三明治面板;近似分析模型;热行为;消融;

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