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首页> 外文期刊>Journal of Spacecraft and Rockets >Themal analysis and Design Optimization of Multilayer Insulation for Reentry Aerodynamic Heating
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Themal analysis and Design Optimization of Multilayer Insulation for Reentry Aerodynamic Heating

机译:再入式气动加热多层保温材料的热分析和设计优化

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摘要

A design-of-experiment technique was used to investigate optimum design of multilayer insulations for reentry aerodynamic heating. Combined radiation/conduction heat transfer in high-temperature multilayer insulations was modeled using a finite volume numerical model, which was validated by comparison with steady-state effective thermal conductivity measurements, and transient thermal tests simulating reentry aerodynamic heating condi- tions. It was found the use of 2-mm foil spacing and locating the foils near the ht boundary, with the top foil 2 mm away from the hot boundary, resulted in the most effective insulation design.
机译:实验设计技术用于研究用于再入空气动力加热的多层绝热材料的最佳设计。使用有限体积数值模型对高温多层绝缘中的辐射/传导组合传热进行建模,该模型通过与稳态有效导热率测量和模拟折返空气动力加热条件的瞬态热测试进行比较而得到验证。发现使用2 mm的箔间距,并将箔定位在ht边界附近,顶部箔距热边界2 mm,这导致了最有效的隔热设计。

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