1. 中国空气动力研究与发展中心 气动噪声控制重点实验室,四川,绵阳,621050
2. 中国空气动力研究与发展中心 结冰与防除冰重点实验室,四川,绵阳,621050
3. 澳大利亚新南威尔士大学 机械与制造工程学院,悉尼,2052
张军(1983-), 男, 四川简阳人, 助理研究员, 主要从事气动噪声产生机理与控制方法研究.E-mail:jzhang@nudt.edu.cn
纸质出版:2020
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张军, 张俊龙, 雷红胜, 赵维明, DoolanCon.. 基于隐式温度修正的二维热线风速仪校准方法[J]. 空气动力学学报, 2020, 38(1): 43-47, 65.
ZHANG Jun, ZHANG Junlong, LEI Hongsheng, et al. A cross-hotwire calibration method with implicit temperature correction[J]. 2020, 38(1): 43-47, 65.
张军, 张俊龙, 雷红胜, 赵维明, DoolanCon.. 基于隐式温度修正的二维热线风速仪校准方法[J]. 空气动力学学报, 2020, 38(1): 43-47, 65. DOI: 10.7638/kqdlxxb-2019.0063.
ZHANG Jun, ZHANG Junlong, LEI Hongsheng, et al. A cross-hotwire calibration method with implicit temperature correction[J]. 2020, 38(1): 43-47, 65. DOI: 10.7638/kqdlxxb-2019.0063.
热线风速仪主要用于湍流流场测量。热线测量的主要误差来源是由环境温度变化导致的热线校准参数的变化。Brunn提出的传统温度效应修正方法在环境温度变化较大的情况下会带来明显的误差。本文经过理论推导,提出了一种新的基于隐式温度修正的二维热线风速仪校准方法,并开展了热线校准实验研究。结果表明:当环境温度变化在4℃范围内时,本文提出的方法与Brunn方法的测量精度相当;当环境温度变化超过4℃时,本文提出的方法的测量精度远高于Brunn方法。
Hotwire anemometry is mainly used for turbulence measurement. The main source of error for hot-wire anemometry is the variation of ambient temperature. The most popular temperature correction method was given by Brunn. However
the measurement error is large once the temperature variation exceeds several degrees. In this study
a new cross-hotwire calibration method was proposed
and the temperature correction was implicitly considered. Experimental studies were performed to validate the proposed method. The results show that:1) when the temperature variation was less than 4℃
no obvious difference was observed between the present method and Brunn's method; 2) when the temperature variation was larger than 4℃
the accuracy of the present method was more accurate than Brunn's method.
BRUNN H H. Hot-wire anemometry[M]. Oxford: Oxford University Press, 1995.
HENBEST S M, JONES M B, WATMUFF J H. A technique for rapid calibration of cross-hot-wires[C ] //20 th Australian Fluid Mechanics Conference, Perth, Australia, 5-8 December 2016.
WALKER D A, WALKER M D. Experimental comparison of two hot-wire techniques in supersonic flow[J]. AIAA Journal, 1988, 27(8): 1074-1080.
LUEPTOW R M, BREUER K S, HARITONIDIS J H. Computer-aided calibration of X-probes using a look-up table[J]. Experiments in Fluids, 1988, 6: 115-118.
MA H S, SHI P J, LI X C, et al. Investigation of calibration method for hot-wire probe incompressible flow[J]. Acta Aerodynamica Sinca, 2019, 37(1): 55-60.
JORGENSEN F E. How to measure turbulence with hot-wire anemometers-a practical guide[R]. Dantec Dynamics, Denmark, 2002.
MORO J P, VUKOSLAVCEVIC P V, BLET V. A method to calibrate a hot-wire X-probe for applications in low-speed, variable-temperature flow[J]. Meas Sci Technol, 2003, 14: 1054-1062.
BRUNN H H, TROPEA C. Thecalibration of inclined hot-wires probes[J]. J Phys E: Sci Instrum, 1985, 18: 405-412.
WESTPHAL R V, MEHTA R D. Crossed hot-wire data acquisition and reduction system[R]. NASA TM-85881, 1984.
BRUNN H H, NABHANI N, FARDAD A A, et al. Calibraton and analysis of X hot-wire probe signals[J]. Meas Sci Technol, 1990, 1:782-785.
YASA T, PANIAAGUA G, DENOS R. Hot-wire anemometry for non-isothermal flows and effect of aging of the sensor wire[R]. Data acquisition and signal processing for turbomachinery applications Von Karman Institute for Fluid Dynamics, 2005.
CUKUEL B, ACARER S, ARTS T. A novel perspective to high-speed cross-hot-wire calibration methodology[J]. Exp Fluids, 2012, 53:1073-1085.
MARCUS H, ALEXANDER S. Temperature corrections for constant temperature and constant current hot-wire anemometry[J]. Meas Sci Technol, 2010, 21:10540.
COME B, SARMA G R. Constant voltage anemometer practice in supersonic flows[J]. AIAA Journal, 2001, 39:261-270.
SARMA G R. Automated constant voltage anemometer for measurements with fluid temperature drift[J]. Review of Scientific Instruments, 2002, 73:1313.
COLLIS D C, WILLIAMS M J. Two-dimensional convection from heated wires at low Reynolds numbers[J]. Journal of Fluid Mechanics, 1959, 6:357-384.
ALEXANDER S, MARK Z. Applications of dense gases to model testing for aeronautical and hydrodynamic applications[J]. Meas Sci Technol, 2005, 16:1710-1715.
ZHANG J, WANG X N, ZHANG J L, et al. A study of shear-layer corrections and a tensioned fabric wall for the localization of sound sources in wind tunnel[C]//The 25th AIAA/CEAS aeroacoustics conference, Delft, the Netherlands, 20-24 May, 2019.
POPE S B. Turbulence flow[M]. United Kingdom:University Cambridge press, 2000.
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