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Finite Element Method for Ablative Thermal Protection Systems Design for Atmospheric Re-Entry Vehicles

机译:大气重新入口车辆消融热保护系统设计有限元方法

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The objective of the present work is to present a numerical procedure developed on the basis of the ANSYS Parametric Design Language to simulate the ablation process and the temperature distribution inside materials subjected to severe heat flux conditions with a Finite Element approach. The thermal properties of P50 ablators has been included in the analysis in order to compare numerical results with the outcomes of an analogous experimental test reported in literature. The numerical tool will be employed to predict the performances of innovative ablative material in course of development and characterization at CIRA for TPS applications.
机译:本作工作的目的是介绍基于ANSYS参数化设计语言开发的数值程序,以模拟消融过程和通过有限元方法对经受严重的热通量条件进行的材料内部的温度分布。 P50烧蚀器的热性能已包括在分析中,以便将数值结果与文献中报告的类似实验试验的结果进行比较。将采用数值工具来预测TPS应用的Cira的开发和表征过程中创新烧蚀材料的性能。

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