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热障涂层厚度的脉冲涡流检测反演方法
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作者 范文茹 昌勇 《计量学报》 CSCD 北大核心 2024年第6期819-826,共8页
针对热障涂层厚度的高精度测量,提出一种脉冲涡流检测反演方法。该方法提出两阶段处理技术对脉冲涡流检测信号进行预处理,采用主成分分析法提取预处理信号的主成分分量,最后构建BP神经网络实现涂层厚度预测。通过COMSOL建模仿真实验证... 针对热障涂层厚度的高精度测量,提出一种脉冲涡流检测反演方法。该方法提出两阶段处理技术对脉冲涡流检测信号进行预处理,采用主成分分析法提取预处理信号的主成分分量,最后构建BP神经网络实现涂层厚度预测。通过COMSOL建模仿真实验证明两阶段处理方法可有效地减小提离效应并区分厚度特征的变化,基于主成分分析的特征提取方法能够对陶瓷层和粘结层厚度变化进行分类识别。结果显示该方法对陶瓷层厚度计算的平均相对误差约为0.4%,对粘结层厚度计算的平均相对误差约为2.6%。可见,该方法对热障涂层厚度的反演精度较高。 展开更多
关键词 厚度计量 热障涂层 脉冲涡流 两阶段处理法 主成分分析 BP神经网络
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基于X射线掠射法的纳米薄膜厚度计量与量值溯源研究 被引量:7
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作者 崔建军 高思田 《物理学报》 SCIE EI CAS CSCD 北大核心 2014年第6期109-116,共8页
为了实现纳米薄膜厚度的高精度计量,研制了可供台阶仪、扫描探针显微镜等接触测量的纳米薄膜样片,研究了X射线掠射法测量该纳米薄膜样片厚度的基本原理和计算方法,导出了基于Kiessig厚度干涉条纹计算膜层厚度的线性拟合公式,并提出了一... 为了实现纳米薄膜厚度的高精度计量,研制了可供台阶仪、扫描探针显微镜等接触测量的纳米薄膜样片,研究了X射线掠射法测量该纳米薄膜样片厚度的基本原理和计算方法,导出了基于Kiessig厚度干涉条纹计算膜层厚度的线性拟合公式,并提出了一种可溯源至单晶硅原子晶格间距和角度计量标准的纳米膜厚量值溯源方法,同时给出了相应的不确定度评定方法.实验证明:该纳米薄膜厚度H测量相对扩展不确定度达到U=0.3 nm+1.5%H,包含因子k=2.从而建立了一套纳米薄膜厚度计量方法和溯源体系. 展开更多
关键词 纳米计量 纳米薄膜厚度 X射线掠射 厚度计量
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Use of Non-uniform Rational B-splines for Discharge Calculation in the Velocity Area Method
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作者 Zbigniew Krzemianowski Adam Adamkowski 《Journal of Energy and Power Engineering》 2014年第5期911-919,共9页
The velocity area method belongs to the group of primary methods for discharge measurement in hydropower plants. The measurements require an appropriate application of measuring devices and carrying out correctly the ... The velocity area method belongs to the group of primary methods for discharge measurement in hydropower plants. The measurements require an appropriate application of measuring devices and carrying out correctly the process of data analyzing including integration technique. The authors present their own experiences gathered during many years of utilizing the current meter method for discharge measurement in many hydropower plants. They have developed the special integration techniques using the progressive numerical algorithms. The techniques differ from the recommendations contained in the relevant international standards. The authors' own software for calculating the discharge from the measured local velocity distribution (obtained using current meters) adopts advanced spline functions, the so-called NURBS (non-uniform rational B-splines). Nowadays, this kind of splines is commonly used in modeling of the complex geometrical shapes because of their smoothness. It is assessed that it represents much better quality of interpolation than the classic spline functions (classic cubic spline technique). Particularly, the better properties of the NURBS splines can be observed for velocity profile area characterized by very strong velocity gradients where boundary layers meet the core regions of the flow (mainstream). In the developed software the boundary layer thickness and exponent of von Karman function is calculated in accordance with the ISO 3354 standard. The software has been successfully used during many performance tests of the hydraulic turbines in Poland for several years. Paper presents the results of flow rate measurements for two different flow systems of Kaplan turbines. First case concerns the application of the current meters in a long circular penstock whereas the second one in short rectangular turbine intake. A comparative analysis of three flow calculation procedures applied for these two cases is presented in the paper-(1) the integration procedure according to the ISO 3354 standard; (2) the integration procedure based on the NS (natural splines); and (3) the integration procedure based on the NURBS. The results obtained using these three procedures for the first case (intake via long circular penstock) were compared with the results of discharge measurements conducted using the pressure-time method. 展开更多
关键词 HYDROPOWER discharge measurements current meter method pressure-time method.
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Study of Choked Flows through a Convergent Nozzle 被引量:2
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作者 Kazunori KUBO Yoshiaki MIYAZATO Kazuyasu MATSUO 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第3期193-197,共5页
When sonic nozzles of significantly smaller diameter are used as standard flow meters,the critical back pressure ratio is affected by the boundary layer at the nozzle throat.However,the effect of the boundary layer on... When sonic nozzles of significantly smaller diameter are used as standard flow meters,the critical back pressure ratio is affected by the boundary layer at the nozzle throat.However,the effect of the boundary layer on choking criteria is still controversial.Then,the choking phenomenon of a convergent nozzle flow has been experimentally investigated using four convergent nozzles with the same diameter followed by a straight pipe of a variable length.As a result,it is shown that the critical back pressure ratio is smaller than that for the steady one-dimensional is-entropic flow and decreases as the boundary layer thickness increases.Moreover,the main flow Mach number at the nozzle exit is supersonic when the back pressure ratio is equivalent to the choking condition,and the Mach number increases as the boundary layer thickness increases. 展开更多
关键词 Boundary Layer Convergent Nozzle Choked Flow Choking Pressure Ratio
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A study of the operating parameters and barrier thickness of Al_(0.08)In_(0.08)Ga_(0.84)N/Al_xIn_yGa_(1-x-y)N double quantum well laser diodes
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作者 A.J.GHAZAI S.M.THAHAB +1 位作者 H.ABU HASSAN Z.HASSAN 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第1期47-51,共5页
The operating parameters such as the internal quantum efficiency (η), internal loss (α) and transparent threshold current density (J0) of double quantum well laser diodes were investigated and identified using... The operating parameters such as the internal quantum efficiency (η), internal loss (α) and transparent threshold current density (J0) of double quantum well laser diodes were investigated and identified using the program, Integrated System Engineering-Technical Computer Aided Design (ISE-TCAD). Various thicknesses (6, 7, 8, 10, 12 rim) of AlxInyGa1-x-yN barriers with (3 nm) Al0.08In0.08Ga0.84N wells as an active region were studied. The lowest threshold current (lth), and the highest output power (Pop) were 116 mA and 196 mW respectively, at barriers thickness of 6 nm, Al mole fraction of 10% and In mole fraction of 1%, at an emission wavelength of 359.6 nm. 展开更多
关键词 AIInGaN QUATERNARY UV laser diode quantum well barrier thickness
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