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The Effect of Diffuser Angle on the Discharge Coefficient of a Miniature Critical Nozzle 被引量:5

The Effect of Diffuser Angle on the Discharge Coefficient of a Miniature Critical Nozzle
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摘要 Many researches on critical nozzles have been performed to accurately measure the mass flow rate of gas flow,and to standardize the performance as a flow meter.Recently,much interest is being paid on the measurement of very small mass flow rate in industry fields such as MEMS applications.However,the design and performance data of the critical nozzles obtained so far have been applied mainly to the critical nozzles with comparatively large diameters,and the works available on miniature critical nozzles are lacking.In the present study,a computational fluid dynamics method has been applied to investigate the influence of the diffuser angle on discharge coefficient of the miniature critical nozzles.In computations,the throat diameter of critical nozzle is varied from 0.2 mm to 5.0 mm and the diffuser angle is changed from 2 deg to 8 deg.The computational results are validated with some experimental data available.The results show that the present computational results predict appropriately the discharge coefficient of the gas flows through miniature critical nozzles.It is known that the discharge coefficient is considerably influenced by the diffuser angle,as the throat diameter of nozzle becomes small below a certain value.This implies that the miniature critical nozzles should be carefully designed. Many researches on critical nozzles have been performed to accurately measure the mass flow rate of gas flow,and to standardize the performance as a flow meter.Recently,much interest is being paid on the measurement of very small mass flow rate in industry fields such as MEMS applications.However,the design and performance data of the critical nozzles obtained so far have been applied mainly to the critical nozzles with comparatively large diameters,and the works available on miniature critical nozzles are lacking.In the present study,a computational fluid dynamics method has been applied to investigate the influence of the diffuser angle on discharge coefficient of the miniature critical nozzles.In computations,the throat diameter of critical nozzle is varied from 0.2 mm to 5.0 mm and the diffuser angle is changed from 2 deg to 8 deg.The computational results are validated with some experimental data available.The results show that the present computational results predict appropriately the discharge coefficient of the gas flows through miniature critical nozzles.It is known that the discharge coefficient is considerably influenced by the diffuser angle,as the throat diameter of nozzle becomes small below a certain value.This implies that the miniature critical nozzles should be carefully designed.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第3期222-227,共6页 热科学学报(英文版)
关键词 喷嘴直径 扩散角 微型 临界 质量流量 放电 流动性能 计算系数 Compressible Flow, Critical Nozzle, Compressible Flow, Discharge Coefficient, Diffuser Configuration, Reynolds Number
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参考文献13

  • 1Tang, S. E, and Fenn, J. B., "Experimental Determination of the Discharge Coefficients for Critical Flow Through an Axisymmetric Nozzle," AIAA Journal, Vol. 16, No. 1, 1978, pp. 41-46.
  • 2Kim, H. D., Kim, J. H., Park, K. A., Setoguchi, T., and Matsuo, S., "Computational Study of the Gas Flow Through a Critical Nozzle," IMechE Journal of Mechanical Engineering Science, Vol. 217, 2003, pp. 1179- 1189.
  • 3Arnberg, B. T., Britton, C. L., and Seidel, W. F., "Discharge Coefficient Correlations for Circular Arc Venturi Flow Meters at Critical(Sonic) Flow," ASME, 1973, 73- WA/FM-8.
  • 4Kim, H. D., Kim, J. H., and Park, K. A., "Study for the Gas Flow Through a Critical Nozzle," Proceedings of ASME FEDSM'03 4th ASME JSME Joints Fluids Engineering Conference, Hawaii, 2003, FEDSM2003-45593.
  • 5Kim, J. H., Kim, H. D,, and Park, K. A., "Computational/Experimental Study of a Variable Critical Nozzle Flow," Flow Measurement and Instrumentation, Vol. 17, No. 2, 2006, pp. 81-86.
  • 6Bignell, N., "The Use of Small Sonic Nozzles at Low Reynolds Numbers," Flow Measurement and Instrumentation, Vol. 7, 1996, pp. 77-83.
  • 7Choi, Y. M., Park, K. A., Park, J. T., Choi, H. M., and Park, S. O., "Interference Effects of Three Sonic Nozzles of Different Throat Diameters in the Same Meter Tube," Flow Measurement and Instrumentation, Vol. 10, 1999, pp. 175-181.
  • 8Kim, H. D., Kim, J. H., Park, K. A., Setoguchi, T., and Matsuo, S., "Study of the Effects of Unsteady Downstream Conditions on the Gas Flow through a Critical Nozzle," IMechE Journal of Mechanical Engineering Science, Vol. 218, 2004, pp. 1163-1173.
  • 9Kim, J. H., Kim, H. D., Park, K. A., Setoguchi, T., and Matsuo, S., "A Fundamental Study of a Variable Critical Nozzle Flow," Experiments in Fluids, Vol. 40, No. 1, 2006, pp. 127-134.
  • 10Mueller, J., Tang, W. C., Wallace, A. E, Li, W. J., Bame,D. E, Chakraborty, I. and Lawton, R. A., "Design, Analysis and Fabrication of a Vaporizing Liquid Micro-Thruster," Proceedings of 33rd AIAA Joint Propulsion Conf., 1997, pp. 1-10.

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