太空服的热绝缘性能的数值建模
Michał Dzięgielewski1, Ryszard Korycki2, Halina Szafrańska3
1Faculty of Material Technologies and Textile Design, Lodz University of Technology, Zeromskiego, 116, 90-924 Lodz, Poland.
Materials (Basel, Switzerland)
|April 9, 2024
概括
这项研究使用计算机模拟和物理模型模拟太空服的隔热. 热微流星的服装 热微流星服装
科学领域:
- 材料科学 材料科学 材料科学
- 航空航天工程 航空航天工程
- 热力工程是热力工程中的一个.
背景情况:
- 太空服需要先进的隔热.
- 热微流星服 (TMG) 对于温度调节至关重要.
- 了解TMG材料的特性对于宇航员的安全至关重要.
研究的目的:
- 为了模拟一个多层空间服材料的隔热性能.
- 用计算机模拟和数学模型进行热分析.
- 评估一个示例的材料布置适用于太空应用的适用性.
主要方法:
- 采用计算机模拟技术和基于物理的数学模型.
- 使用Ansys工作台软件进行数值建模.
- 应用有限元法 (FEM) 进行结构分析.
主要成果:
- 模拟了TMG材料布置中的温度场.
- 将模拟结果与数学模型的验证计算进行比较.
- 评估了开发模型的质量和潜在的差异.
结论:
- 验证了示例太空服材料的绝热性能.
- 证实了所使用的模拟和数学模型的可靠性.
- 提供了支持该材料用于宇航员热保护的数据.
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