Three-dimensional thermal boundary layer corrections for circular heat flux gauges mounted in a flat plate with a surface temperature discontinuity

被引:9
|
作者
Kandula, M. [1 ]
Haddad, G. F.
Chen, R. -H.
机构
[1] Sierra Lobo Inc, Kennedy Space Ctr, FL 32899 USA
[2] NASA, Kennedy Space Ctr, FL 32899 USA
[3] Univ Cent Florida, Mech Mat & Aerosp Engn Dept, Orlando, FL 32816 USA
基金
美国国家航空航天局;
关键词
convective heat flux gauges; surface temperature discontinuity; three-dimensional thermal boundary layers;
D O I
10.1016/j.ijheatmasstransfer.2006.07.008
中图分类号
O414.1 [热力学];
学科分类号
摘要
Three-dimensional Navier-Stokes computational fluid dynamics (CFD) analysis has been performed in an effort to determine thermal boundary layer correction factors for circular convective heat flux gauges (such as Schmidt-Boelter and plug type) mounted flush in a flat plate subjected to a stepwise surface temperature discontinuity. Turbulent flow solutions with temperature-dependent properties are obtained for a freestream Reynolds number of 1E6, and freestream Mach numbers of 2 and 4. The effect of gauge diameter and the plate surface temperature have been investigated. The 3D CFD results for the heat flux correction factors are compared to quasi-2D results deduced from constant property integral solutions and also 2D CFD analysis with both constant and variable properties. The role of three-dimensionality and of property variations on the heat flux correction factors has been demonstrated. (c) 2006 Elsevier Ltd. All rights reserved.
引用
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页码:713 / 722
页数:10
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