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Correction for effect of temperature-dependent diffusivity on temperature-sensitive-paint heat-flux measurement

机译:校正温度相关扩散率对热敏涂料热通量测量的影响

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摘要

A simple method is developed for correcting the effect of the temperature-dependent thermal diffusivity on temperature-sensitive-paint (TSP) heat flux measurements in hypersonic wind tunnels. The relation between the heat flux obtained using the constant thermal diffusivity and the heat flux obtained using the temperature-dependent diffusivity is discussed based on an analysis of the nonlinear heat conduction equation. The non-dimensional correction factor is introduced and modeled as an approximate function of the measured surface temperature for the monotonically increasing heat flux histories, which can be determined in situ using the data at several selected points. The corrected heat flux field is obtained by multiplying the correction factor field with the heat flux field obtained using the analytical inverse heat transfer method for constant thermal properties. This method is validated through simulations. (C) 2019 Elsevier Ltd. All rights reserved.
机译:开发了一种简单的方法来校正与温度有关的热扩散率对高超声速风洞中的热敏涂料(TSP)热通量测量的影响。基于非线性热传导方程的分析,讨论了使用恒定热扩散率获得的热通量和使用随温度变化的扩散率获得的热通量之间的关系。引入无量纲校正因子并将其建模为单调递增的热通量历史记录的测得表面温度的近似函数,可以使用几个选定点的数据就地确定该值。通过将校正因子场乘以使用解析逆热传递方法获得的恒定热特性的热通量场,可以得到校正后的热通量场。通过仿真验证了该方法。 (C)2019 Elsevier Ltd.保留所有权利。

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