传热
材料科学
薄膜温度
薄膜
边界层
灵敏度(控制系统)
湍流
量具(枪械)
蒸发
传热系数
复合材料
机械
光学
热力学
电子工程
雷诺数
物理
纳米技术
工程类
冶金
努塞尔数
作者
Masanori Hayashi,Akira Sakurai,Shigeru Aso
出处
期刊:The Journal of the Japan Society of Aeronautical Engineering
[Japan Society for Aeronautical and Space Sciences]
日期:1985-01-01
卷期号:33 (380): 525-531
被引量:1
标识
DOI:10.2322/jjsass1969.33.525
摘要
A new method of measuring heat transfer rate with high spatial resolution and fast response is developed to be used in wind tunnels with long flow duration. For the development of the new method a multi-layered thin film heat transfer gauge is proposed. The principle of the sensor is based on measuring the temperature gradient across a thin, heat resistant layer of SiO with two, thin film resistance thermometers on its upper and lower surfaces. These thin films and the heat resistant layer are deposited by vacuum evaporation technique. The design consideration, the accuracy of the sensor, frequency response, and the calibration technique are discussed. The sensor is applied to the measurement of the heat transfer rate in turbulent boundary layer on a flat plate at Mach number 4, Tw/T0= 0.64, and Re=1.4×107, and shows high sensitivity and fast response. It also shows excellent durability.
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