The error compensation method of the low-speed wind tunnel flow temperature based on the thermocouple

被引:0
作者
Yang Z. [1 ]
Gu Z. [1 ]
Zhang W. [1 ]
Zeng X. [1 ]
机构
[1] Facility Design and Instrumentation Institute of China Aerodynamics Research and Development Center, Mianyang
来源
Yi Qi Yi Biao Xue Bao/Chinese Journal of Scientific Instrument | 2022年 / 43卷 / 05期
关键词
Heat conduction error; Low-speed airflow; Radiation error; Thermocouple;
D O I
10.19650/j.cnki.cjsi.J2108335
中图分类号
学科分类号
摘要
The quality of flow temperature data in the low-speed wind tunnel is the key to the character of the flow field of the wind tunnel. This article carries out special research on the compensation method of thermal conductivity error and radiation error in thermocouple measurement. Based on the basic principles of heat transfer, research is implemented on the method of the thermal conductivity error compensation with the fixed value of the immersed length of the thermocouple wire and the method of the radiation error compensation with the fixed value of relative change rate of the surrounding temperature. Simulation results of the quantitative relationship between the immersed length of the thermocouple, the relative change rate of the surrounding temperature, and temperature error are obtained. To evaluate the error mechanism analysis and simulation results, a wind tunnel validation test is carried out. Test results show that the measured thermocouple immersion error results are consistent with the theoretical simulation results, and the relative change rate of surrounding temperature ω<1 can significantly reduce the influence of temperature measurement radiation error, which can reduce the influence of temperature measurement radiation error on temperature uniformity by 7.12 times. The method presented in this article provides useful exploration and technical basis for the engineering application of the thermocouple in gas medium. © 2022, Science Press. All right reserved.
引用
收藏
页码:68 / 76
页数:8
相关论文
共 23 条
  • [11] YANG ZH X, ZENG X, ZHANG W Q., Dynamic. characteristics of thermocouple in gas medium, Journal of Aerospace Power, 35, 12, pp. 2514-2520, (2020)
  • [12] ZOU Y., Research on compensation temperature of the working copper/copper-nickel thermocouple, Metrology and Measurement Technique, 47, 9, pp. 5-7, (2020)
  • [13] JIN M J, LI W J, ZHENG Y J, Et al., Autoregressive model with exogenous input of thermocouple dynamic response, Chinese Journal of Sensors and Actuators, 32, 6, pp. 844-851, (2019)
  • [14] PAN B Q, LI Y F, ZHANG ZH J., Study on dynamic calibration and dynamic compensation technique of the thermocouple based on quantum-behaved particle swarm algorithm, Chinese Journal of Sensors and Actuators, 28, 7, pp. 992-996, (2015)
  • [15] CUI Y X, XUE SH J, DU P, Et al., Research on preparation and milling application of high performance thin film thermocouple, Chinese Journal of Sensors and Actuators, 41, 4, pp. 32-40, (2020)
  • [16] GUAN P, AI Y T, XU Y, Et al., Numerical study on the effect of thermocouple mounting coating on temperature measurement of nozzle guide vane, Journal of Northwestern Polytechnical University, 38, 1, pp. 95-103, (2020)
  • [17] LIU B, WANG CH Y, HE Y X., Uncertainty evaluation on thermocouple's time constant, Chinese Journal of Sensors and Actuators, 33, 5, pp. 666-669, (2020)
  • [18] YANG W P, ZHANG W H, ZOU ZH P, Et al., Steady state error estimation and modification of a shielded thermocouple, Journal of Aerospace Power, 33, 11, pp. 2784-2795, (2018)
  • [19] CAI J, YANG Y J, LIAO L, Et al., Conductive error influence on temperature measurement, Journal of Beijing University of Aeronautics and Astronautics, 34, 11, pp. 1353-1363, (2008)
  • [20] YANG C, WU W L, XIONG Y B, Et al., Calibration technology of high-temperature thermocouple for combustor exit of an aero-engine, Journal of Aerospace Power, 31, 4, pp. 769-774, (2016)