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关于单元表面吸收率的系统温度误差计算
引用本文:张伟清,宣益民,韩玉阁.关于单元表面吸收率的系统温度误差计算[J].中国空间科学技术,2006,26(4):42-47.
作者姓名:张伟清  宣益民  韩玉阁
作者单位:南京理工大学动力工程学院,南京,210094
摘    要:利用系统灵敏度理论和系统误差统计理论,通过引入辐射传递系数和角系数间的关系,针对漫发射、漫反射热系统,提出了关于单元表面吸收率的系统温度误差计算方法。以立方体内表面间的辐射换热为例,采用该计算方法对系统温度误差进行了计算。通过分析比较表明:采用该方法得到系统温度灵敏度具有较高计算精度,系统统计温度误差受实验次数影响,并且在均方差较小的情况下,系统统计温度误差之比等于系统温度灵敏度之比的绝对值。

关 键 词:系统温度误差  灵敏度  系统  热分析  航天器
收稿时间:2005-04-01
修稿时间:2005-04-012005-06-20

Computation of System Temperature Error about Unite Surface Absorptivity
Zhang Weiqing,Xuan Yimin,Han Yuge.Computation of System Temperature Error about Unite Surface Absorptivity[J].Chinese Space Science and Technology,2006,26(4):42-47.
Authors:Zhang Weiqing  Xuan Yimin  Han Yuge
Institution:School of Power Engineering, Nanjing University of Science and Technology, Nanjing 210094
Abstract:Based on system sensitivity theory and system error analysis theory,by introducing the relation between radiation transfer coefficient and angle factor,a computational method,which computes system temperature error about unite surface's absorptivity is developed.Taking the(example) of radiation transfer among surfaces inside a cubic,system temperature error is computed by the computional method.It shows that system temperature sensitivity has higher precision,and experimental time influences on system statistical temperature error.If standard deviation is(smaller),ratio of system statistical temperature error is equal to ratio of system temperature(sensitivity).
Keywords:System temperature error Sensibility System Thermal analysis Spacecraft
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