参数可变的拉伸/收缩翅片中的温度分布

IF 2.8 Q2 THERMODYNAMICS
Heat Transfer Pub Date : 2024-06-14 DOI:10.1002/htj.23103
Priti Sharma, Surjan Singh, Subrahamanyam Upadhyay
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引用次数: 0

摘要

在本文中,我们考虑了一个数学模型,该模型在具有指数曲线的拉伸/收缩直翅片中具有独特的传热机制。热导率、内部发热量和传热系数都与温度有关。热量通过对流和辐射暴露到周围环境中。控制微分方程和边界条件以无量纲形式表示。在我们的研究中,我们考虑了可变的表面发射率(即常数)和温度的线性函数。对流传热参数被视为低功率类型。这项工作的新颖之处在于应用了随温度变化的表面发射率,并通过 Legendre 小波配位法解决了问题。本研究结果与之前研究结果的对比分析以表格形式呈现,以供验证,结果完全相同。不同变量的影响以图表形式呈现,并进行了详细讨论。本分析侧重于实际应用,为改进翅片设计提供了宝贵的见解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Temperature distribution in stretching/shrinking fin with variable parameters

In this paper, we consider a mathematical model, which has a unique mechanism of heat transfer in the stretching/shrinking straight fin with an exponential profile. The thermal conductivity, internal heat generation, and heat transfer coefficient are considered temperature-dependent. Heat is exposed to the surroundings by convection and radiation. The governing differential equation and boundary conditions are presented in a dimensionless form. In our study, we considered variable surface emissivity, that is, a constant, and the linear function of a temperature. The convective heat transfer parameter is considered a power-low type. The novelty of this work is the application of temperature-dependent surface emissivity, and the problem is solved by the Legendre wavelet collocation method. A comparative analysis of the present results in the context of previous findings is presented in the form of a table for validation and found exactly the same. The impacts of distinct variables are presented in the form of figures and discussed in detail. The present analysis is focused on real-world applications and offers valuable insights for improving the design of fins.

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来源期刊
Heat Transfer
Heat Transfer THERMODYNAMICS-
CiteScore
6.30
自引率
19.40%
发文量
342
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