且偏差达到1.0%时个别反演数据明显“失真”.③ k 反演计算误 差的标准差 y 与实验偏差 γ 满足 y =2285.2 γ2- 10.484 γ +0.0037的关系式; n 反演计算误差的标准差受实验偏差影响较小
但偏差导致反演 n 误差均超过20%.
Abstract
The spectral transmittance radio calculation model of glass- liquid hydrocarbon fuel-glass three layer slabs was developed based on ray trace method
and an inverse model was built to determine the thermal radiation property (k is extinction coefficient and n is refractive index) of liquid hydrocarbon fuel in the three layer slabs.The inverse model was retrieved
and was combined with Monte-Carlo method and area approach method.The thermal radiation property of heptane attained in the references was selected as the true values
and the spectral transmittance radio of the three layer slabs based on the direct model simulation was regarded as the experimental values.The thermal radiation property of Heptane was achieved by the inverse model
and then the effect of measurement error on the inverse results was also investigated.The results show that
(1) the standard deviation of k calculation error by the inverse model is less than 0.003%
and that of n is higher than 21%. (2) the effect of measurement error on the inverse results is urgent distinct
and some inversed calculation values are obviously when the measurement error is higher than 1%.(3) the standard deviation of k calculation error and measurement error y satisfy the equation which is y =2285.2 γ2-10.484 γ +0.0037.The effect of measurement error on the standard deviation of n calculation error is lower
however
the n calculation error is higher than 20% when the measurement error exists.
Effect of channel cross sectional shape on flow distribution of hydrocarbon fuel
Thermal cracking and heat transfer of hydrocarbon fuel with catalytic steam reforming
Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes
组合式弹性金属密封泄漏特性实验研究与结构优化
基于自适应MOMEDA滚动轴承故障特征提取方法
Related Author
张晓红
姜俞光
秦江
鲍文
张定瑞
张枭雄
侯凌云
ZHANG Bin
Related Institution
西北工业大学 动力与能源学院
哈尔滨工业大学 能源科学与工程学院
清华大学 航天航空学院
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermcolynamics, School of Jet Propulsion, Beijing University of Aeronautics Astronautics