期刊文献+

叶轮出口总温总压测量用单热膜吸气探针的研究 被引量:1

A SINGLE HOT-FILM ASPIRATING PROBE FOR MEASURING THE TOTAL TEMPERATURE AND PRESSURE AT THE OUTLET OF IMPELLERS
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摘要 在完整地分析热丝工作关系式的基础上,设计了一种用于周期性动态温度测量的单热膜吸气探针,进行了稳态校准实验和频响检测实验,得到了与理论分析良好一致的探针输出对温度和压力的变化特性,通过严格的标定,可以做到探针测量精度在1%以内。探针的频响至少可达20kHz。用该探针成功测出了一台低压离心风机叶轮出口的温度分布,表明这种探针以其高频响和足够高的灵敏度适用于叶轮机械转子出口温度分布测量。 Based on the analysis of hot-wire operating equations, a high frequency response singlefilm aspirating probe for measuring the time-solved total temperature and pressure in the periodical unsteady flow field is designed. The static calibration of the probe performed in a temperature-pressure adjustable wind tunnel shows that the measuring error can be controlled in 1%. The dynamic calibration conducted in a rotating disc calibration system indicates that the probe has frequency response of over 20 kHz. The probe was used to measure the flow field at the exit of a centrifugal compressor with high sensitivity.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 1999年第5期563-567,共5页 Journal of Engineering Thermophysics
基金 国家攀登计划项目 航空预研项目
关键词 叶轮机 温度 压力 动态测量 热丝 探针 turbomachine, temperature, pressure, dynamic measurement, hot wire
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参考文献3

  • 1蒋浩康,航空动力学报,1992年,7卷,2期
  • 2彭建,航空动力学报,1992年,7卷,3期
  • 3Jiang H K,Proc Int Conf Fluid Dynamic Measurement and Its Applications,1989年,428页

同被引文献14

  • 1Sieverding C H, Arts T, Denos R, et al. J F Measure Techniques for Unsteady Flows in Turbomachines [J]. Ex- periments in Fluids, 2000, 28(4): 285-321.
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  • 4Ng W F, Epstein A N. Unsteady Losses in Transonic Com- pressors [J]. ASME Journal of Engineering Gas hrbines Power, 1985, 107:345-353.
  • 5Mansour M. A 48 kHz Bandwidth, 1.8 mm Diameter En- tropy Probe for Aerothermal Loss Measurements in Tur- bomachinery Flows [D]. Swiss Federal Institute of Tech- nology Zurich, 2009.
  • 6Mansour M, Chokani N, Kalfas A I, et al. Time-Resolved Entropy Measurements Using a Fast-reponse Entropy Probe [J]. Measurement Science 8 Technolog:, 2008, 19: 115041.
  • 7Vukoslav P V, Wallace J M. The Simultaneous Measure- ment of Velocity and Temperature in Heated rbulent Air Flow Using Thermal Anemometry [J]. Measurement Science & Technology, 2002, 13:1615-1624.
  • 8Buttsworth D R, Jones T V. A Fast-Response Total Temperature Probe for Unsteady Compressible Flows [J]. Journal of Engineering for Gas Turbines and Power, 1998, 120:694-702.
  • 9Buttsworth D R, Jones T V, Chana K S. Unsteady To- tal Temperature Measurements Downstream of a High- Pressure Turbine [J]. ASME Journal of Turbomachinery, 1998, 120:760-767.
  • 10Buttsworth D R, Jones T V. A Fast-Response High Spa- tial Resolution Total Temperature ProbeUsing a Pulsed Heating Teachnique [J]. Journal of Turbomachiimry, 1998, 120:601-607.

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