流体力学与飞行力学

可压缩流体恒温热线风速仪校准方法

  • 杜钰锋 ,
  • 林俊 ,
  • 马护生 ,
  • 梁锦敏
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  • 中国空气动力研究与发展中心, 绵阳 621000

收稿日期: 2016-07-12

  修回日期: 2016-10-29

  网络出版日期: 2016-11-21

Calibration method for constant temperature hot-wire anemometer for compressible fluid

  • DU Yufeng ,
  • LIN Jun ,
  • MA Husheng ,
  • LIANG Jinmin
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  • China Aerodynamics Research and Development Center, Mianyang 621000, China

Received date: 2016-07-12

  Revised date: 2016-10-29

  Online published: 2016-11-21

摘要

开展了恒温(CT)热线风速仪校准方法的研究,以满足可压缩流体中湍流度测量需求。将对数函数与多元回归技术相结合,建立了恒温热线风速仪校准的数学模型,并进行了风洞湍流度测量试验验证。在马赫数Ma=0.3~0.55范围内进行了校准试验,根据建立的数学模型对试验数据进行拟合,拟合优度R2=0.999 82,平均绝对速度偏差u=0.18 m/s ,基本满足了恒温热线风速仪校准精度要求。对马赫数Ma=0.55条件下流场进行了湍流度测量,速度测量偏差为0.034%,流场湍流度Tu=0.14%。试验结果证明了恒温热线风速仪应用于可压缩流体速度测量的可行性。

本文引用格式

杜钰锋 , 林俊 , 马护生 , 梁锦敏 . 可压缩流体恒温热线风速仪校准方法[J]. 航空学报, 2017 , 38(6) : 120600 -120600 . DOI: 10.7527/S1000-6893.2016.0283

Abstract

Turbulence level measurement is vital for the research on compressible fluid. Research on calibration method of constant temperature (CT) hot-wire anemometer is carried out. We build a calibration mathematical model for CT anemometer by combining the logarithmic function with the multiple regression technique, and conduct wind tunnel tests on turbulence level measurement to verify the model. Calibration tests are conducted with Mach number varying from 0.3 to 0.55, and data fitting is based on the mathematical model proposed. The results show that the correlation coefficient is R2=0.999 82 and the absolute deviation of velocity in average is u=0.18 m/s, basically meeting the accuracy requirements of CT anemometer calibration. The turbulence level is measured at Ma=0.55. The deviation of velocity measurement is 0.034%, and the turbulence level is Tu=0.14%. The results verify the feasibility of the application of CT anemometer in velocity measurement of the compressible fluid.

参考文献

[1] BRUUN H H. Hot-wire anemometry: Principles and signal analysis[M]. New York: Oxford University Press, 1995: 1-5.
[2] KING V L. On the convection of heat from small cylinders in a stream of fluid: Determination of the convection constants of small platinum wires with application to hot-wire anemometry[J]. Philosophical Transactions of the Royal Society A—Mathematical Physical and Engineering Science, 1914, 214: 373-432.
[3] DRYDEN H L, KUETHE A M. The measurement of fluctuations of air speed by the hot-wire anemometer: NACA-REPORT-320[R]. Washington, D.C.: NACA, 1930.
[4] WESKE J R. A hot-wire circuit with very small time lag: NACA-TN-881[R]. Washington, D.C.: NACA, 1943.
[5] KOVASZNAY L S G. The hot-wire anemometer in supersonic flow[J]. Journal of the Aeronautical Sciences, 1950, 17(9): 565-572.
[6] LAURENCE J C, LANDES L G. Auxiliary equipment and techniques for adapting the constant-temperature hot-wire anemometer to specific problems in air-flow measurements: NACA-TN-2843[R]. Washington, D. C.: NACA, 1952.
[7] QUIX H, QUEST J, BRZEK C. Hot-wire measurements in cryogenic environment: AIAA-2011-0880[R]. Reston: AIAA, 2011.
[8] JAFFA N, MORRIS S, CAMERON J. Phase resolved hot-wire measurements for high speed turbomachinery flows: AIAA-2014-3437[R]. Reston: AIAA, 2014.
[9] STRUK P M, RIGBY D L, VENKATARAM K. A thermal analysis of a hot-wire probe for icing applications: AIAA-2014-2331[R]. Reston: AIAA, 2014.
[10] TORRANCE M C, NATSUI G, RICKLICK M A, et al. Hot-wire study on the impact of porous structure on mean and turbulent velocity profiles in the near-field of a high aspect ratio porous filled slot jet: AIAA-2011-5914[R]. Reston: AIAA, 2011.
[11] HODGES J, NATSUI G, RICKLICK M A, et al. Hot-wire study on the mean and turbulent streamwise velocity profiles following an axisymmetric annular jet: AIAA-2013-3693[R]. Reston: AIAA, 2013.
[12] 汪健生, 郑杰, 舒玮. 用热线风速仪同时测量流场速度与温度[J]. 实验力学, 1998, 13(3): 393-398. WANG J S, ZHENG J, SHU W. Measuring the velocity and the temperature in a flow field at the same time with hot-wire anemometer[J]. Journal of Experimental Mechanics, 1998, 13(3): 393-398 (in Chinese).
[13] 吴志军, 尹程秋. 运用热线风速仪研究内燃机的流动特性[J]. 吉林工业大学自然科学学报, 1999, 29(2): 91-95. WU Z J, YIN C Q. Research of flow characteristics in internal combustion engine with hot wire anemometer[J]. Journal of Jilin University of Technology (Natural Science), 1999, 29(2): 91-95 (in Chinese).
[14] 王仑, 周远, 候宇葵. 热线风速仪低温测速的初步研究[J]. 真空与低温, 2001, 7(2): 89-91. WANG L, ZHOU Y, HOU Y K. Exploration of measuring velocity with constant temperature anemometer system under low temperature condition[J]. Vacuum & Cryogenics, 2001, 7(2): 89-91 (in Chinese).
[15] 黄甫凯林, 徐璋, 张雪梅, 等. 热线风速仪在测量电站风量中的实验研究[J]. 电站系统工程, 2009, 25(3): 17-19. HUANGPU K L, XU Z, ZHANG X M, et al. Experimental study on hot wire anemometer for measurement of power plant airflow[J]. Power System Engineering, 2009, 25(3): 17-19 (in Chinese).
[16] 论立勇, 陈厚磊, 蔡京辉. 高压交变流动下热线风速仪标定方法研究[J]. 实验流体力学, 2010, 24(3): 87-91. LUN L Y, CHEN H L, CAI J H. Investigation on calibration method of hot-wire anemometer in high pressure reciprocating flow[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(3): 87-91 (in Chinese).
[17] 姚惠元, 刘国政, 孙楠, 等. 恒温热线风速仪的一种新型校准方法[J]. 现代电子技术, 2013, 36(23): 110-112. YAO H Y, LIU G Z, SUN N, et al. A new calibration method of constant temperature hot wire anemometer[J]. Modern Electronics Technique, 2013, 36(23): 110-112 (in Chinese).
[18] 秦天超, 马护生, 刘会龙. 热线/热膜探针校准装置结构研制技术总结报告[R]. 绵阳: 中国空气动力研究与发展中心, 2015. QIN T C, MA H S, LIU H L. Summary report of the development of hot-wire/hot-film probe calibration equipment[R]. Mianyang: CARDC, 2015 (in Chinese).
[19] JANSSEN J M L, ENSING L, VANERP J B. A constant temperature operation hot wire anemometer[J]. Proceedings of the IRE, 1959, 46(4): 555-567.
[20] STAINBACK P C, JOHNSON C B. Preliminary measurements of velocity, density and total temperature fluctuations in compressible subsonic flow: AIAA-1983-0384[R]. Reston: AIAA, 1983.

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