三层热保护系统的建模由里曼-利乌维尔分数导数
Rafał Brociek1, Edyta Hetmaniok2, Damian Słota3
1Department of Artificial Intelligence Modelling, Silesian University of Technology, Kaszubska 23, 44-100, Gliwice, Poland.
Scientific reports
|July 29, 2025
概括
这项研究模拟了一个三层热保护系统,使用孔隙材料的微积分计算. 分数导数顺序显著影响热响应,为复杂的传热提供了一个新的模拟工具.
科学领域:
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
- 应用数学 应用数学 应用数学
背景情况:
- 热保护系统 (TPS) 在航空航天应用中至关重要.
- 在多孔材料中建模热传递需要先进的数学方法.
- 分数计算为描述异常扩散和热传导提供了一个强大的框架.
研究的目的:
- 开发和验证一个具有多孔层的三层TPS的数学模型.
- 将里曼-利乌维尔分数导数纳入用于描述多孔层中的热传导.
- 为了调查分数顺序对系统热行为的影响.
主要方法:
- 使用经典和分数顺序的热传导方程开发了一个三层TPS模型.
- 对于多孔层,使用了里曼-利乌维尔分数导数.
- 进行了数值模拟,考虑了热接触电阻和温度依赖性质.
- 为了确保数值的准确性,进行了网状精细化研究.
主要成果:
- 该模型准确地模拟了复杂的TPS结构中的热传导.
- 分数导数顺序 (β) 显著影响温度分布和热反应.
- 数字结果证明了该模型分析短暂热传递的能力.
结论:
- 拟议的分数顺序模型为TPS分析提供了有价值的工具.
- 了解分数顺序的影响对于优化TPS设计至关重要.
- 这项工作为热管理中的先进计算方法奠定了基础.
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