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Numerical Simulation for Thermal Shock Resistance of Thermal Protection Materials Considering Different Operating Environments

机译:不同工作环境下热防护材料抗热震性能的数值模拟

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摘要

Based on the sensitivities of material properties to temperature and the complexity of service environment of thermal protection system on the spacecraft, ultrahigh-temperature ceramics (UHTCs), which are used as thermal protection materials, cannot simply consider thermal shock resistance (TSR) of the material its own but need to take the external constraint conditions and the thermal environment into full account. With the thermal shock numerical simulation on hafnium diboride (HfB2), a detailed study of the effects of the different external constraints and thermal environments on the TSR of UHTCs had been made. The influences of different initial temperatures, constraint strengths, and temperature change rates on the TSR of UHTCs are discussed. This study can provide a more intuitively visual understanding of the evolution of the TSR of UHTCs during actual operation conditions.
机译:基于材料特性对温度的敏感性以及航天器上热保护系统使用环境的复杂性,用作热保护材料的超高温陶瓷(UHTC)不能简单地考虑航天器的抗热震性(TSR)。材料本身,但需要充分考虑外部约束条件和热环境。通过对二硼化((HfB2)进行热冲击数值模拟,详细研究了不同的外部约束条件和热环境对UHTC的TSR的影响。讨论了不同的初始温度,约束强度和温度变化率对UHTC的TSR的影响。这项研究可以提供UHTC的TSR在实际运行条件下的演变的更直观的视觉理解。

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