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On the optimization of circular radiating fins

机译:关于圆形辐射翅片的优化

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摘要

In the present study the optimum dimensions of circular rectangular and triangular profile fins with fin to fin and fin to base radiant interaction are determined. The basic assumptions are one-dimensional heat conduction, and black surface radiation. The governing equations are formulated by means of dimensionless variables and solved numerically. The optimum fm dimensions, bore thickness and height, are presented in generalized dimensionless form. In order to assist the spacecraft thermal systems designers explicit correlations are provided for the dimensionless, bore thickness. The results are analyzed and reported in diagrams that give insight to the operational characteristics of the heat rejection mechanism. Moreover, special attention is given in the error analysis of the numerical methods used, since the accuracy and the reliability of the algorithms employed for the solution of the integro-differential equation is import and for the calculation of the heat dissipation at the fin base and its subsequent optimization.
机译:在本研究中,确定了用翅片与翅片翅片和翅片的圆形矩形和三角形轮廓翅片的最佳尺寸和翅片辐射相互作用。基本假设是一维导热和黑色表面辐射。控制方程通过无量纲变量配制并数值解决。优化的FM尺寸,孔厚度和高度,以广义无量纲形式呈现。为了帮助宇宙飞船热系统设计人员为无量纲,孔厚度提供明确相关性。分析结果,并在图中报道了洞察热排斥机构的操作特性。此外,在所用数值方法的错误分析中给出了特别的注意,因为用于积分微分方程的解决方案的算法的准确性和可靠性是导入的,并且用于计算翅片基底的散热散它随后的优化。

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