中国空气动力研究与发展中心 高速空气动力研究所,四川,绵阳,621000
马护生*(1968-), 男, 陕西周至人, 高级工程师, 研究方向:流动显示与测量技术.E-mail:husheng_ma@163.com
纸质出版:2019
移动端阅览
马护生, 时培杰, 李学臣, 杜钰锋, 任思源, 杜炜. 可压缩流体热线探针校准方法研究[J]. 空气动力学学报, 2019, 37(1): 55-60.
MA Husheng, SHI Peijie, LI Xuechen, et al. Investigation of calibration method for hot-wire probe in compressible flow[J]. 2019, 37(1): 55-60.
马护生, 时培杰, 李学臣, 杜钰锋, 任思源, 杜炜. 可压缩流体热线探针校准方法研究[J]. 空气动力学学报, 2019, 37(1): 55-60. DOI: 10.7638/kqdlxxb-2016.0093.
MA Husheng, SHI Peijie, LI Xuechen, et al. Investigation of calibration method for hot-wire probe in compressible flow[J]. 2019, 37(1): 55-60. DOI: 10.7638/kqdlxxb-2016.0093.
在可压缩流体中利用热线技术进行湍流度测量时,其输出不仅与脉动速度有关,而且也与流体温度、密度紧密相关。因此,需要在与高速可压缩流体特征相似的校准装置中,在使用前对热线探针进行准确校准。本文提出了可压缩流体热线探针校准方法,建立了热线校准(工作)数学模型,并利用自建的热线校准风洞开展了热线校准实验和湍流度测量风洞试验验证,结果表明:热线校准方法可行,校准数学模型合理可靠,热线探针校准精度较高,湍流度测量结果可信,基本可满足高速可压缩流体湍流度测量的工程需要。
The output of hot-wires is related to fluctuation velocities
and is closely related to fluid temperature and density when a hot-wire technology is used to measure turbulence intensity in compressible fluid. Therefore
hot-wire probes should be accurately calibrated before being used in a calibration facility
which has similar characteristics as those in high speed compressible fluid. In this paper
a calibration method for hot-wire probes in compressible flow is proposed
and a mathematical model of hot-wires for calibrations and measurements is established. Calibration experiments of hot-wire probes are conducted
and an experiment of turbulence intensity measurements is carried out in a wind tunnel with self-building hot-wire calibration. The result indicates that
the calibration method is feasible
and the mathematical model is reasonable and reliable. The calibration accuracy for hot-wire probes is high
and the results of turbulence intensity measurements are credible. The engineering requirements for hot-wire probe measurements in compressible flow are basically satisfied.
ZHOU B, TANG G S. Low turbulence intensity and spectrum measurement research in aeroacoustic wind tunnel[J]. Journal of Experiments in Fluid Mechanic, 2015, 29(4):58-64. (in chinese)
JIA Q, YANG Z G, LI Q L. Test research of the flow filed inside the test section of the automative wind tunnel[J]. Journal of Experiments in Fluid Mechanic, 2011, 25(6):33-37. (in chinese)
TIAN Y K, JIANG H. Study on the wake characteristics naval vessels using a hot-wire anemometer in a wind tunnel[J]. Ship Mechanics, 1998, 2(2):13-21. (in chinese)
GAO L M, XI G, WANG S J, et al. Experiment investigation on a vaned diffuser flow filed behind a centrifugal impeller using constant temperature anemometer[J]. Journal of Engineering Thermophysics, 2005, 26(4):559-601. (in chinese)
MO N R. LENG X M. On analysis of single hot wire signals[J]. Journal of Experimental Mechanics, 1997, 12(2):267-273. (in chinese)
WANG J S, ZHENG J, SHU W. Measuring the velocity and 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)
SOUZA F DE, et al. Hot-wire response in high-subsonic flow[R]. AIAA 1999-0310.
JONES G S. Wind tunnel requirements for hot-wire calibration(Invited)[R]. AIAA-1994-2534.
FAVAREGH A L, et al. A new approach for calibration of hot-wires for use in uncertain environments[R]. AIAA 2006-2809.
ZINOVIEV V, LEBIGA V, CHUNG K M, et al. Application of hot-wire technology in a slowdown type transonic wind tunnel[R]. AIAA 2001-0308
NAGABUSHANA K A, STAINBACK P C. A rational technique for calibrating hot-wire probe in subsonic to supersonic speed[R]. AIAA 1994-2536.
STAINBACK P C. Some influences of approximate values for velocity, density, and toal temperature sensitivities on hot-wire anemometer results[R]. AIAA 1986-0506.
HARALD QUIX, JURGEN QUEST, CHRISTIAN BRZEK. Hot-wire measurements in cryogenic environment[R]. AIAA 2011-880.
NICHOLAS JAFFA, SCOTT MORRIS, JOSHUA CAMERON. Phase resolved hot-wire measurements for high speed turbomachinery flows[R]. AIAA 2014-3437.
刘会龙, 马护生, 蒋为民. 热线/热膜探针校准装置气动方案设计[R]. 绵阳:中国空气动力研究与发展中心, 2013.
马护生, 刘会龙, 秦天超. 高速风洞热线/热膜探针校准装置研制及湍流度测量技术初步研究技术总结报告[R]. 绵阳:中国空气动力研究与发展中心, 2015.
0
浏览量
0
下载量
0
CSCD
关联资源
相关文章
相关作者
相关机构
京公网安备11010802024621