期刊文献+

Experimental study on flow and heat transfer characteristics of synthetic jet driven by piezoelectric actuator 被引量:9

Experimental study on flow and heat transfer characteristics of synthetic jet driven by piezoelectric actuator
原文传递
导出
摘要 To investigate the flow and heat transfer characteristics of a synthetic jet driven by piezoelectric actuator, experimental investigation utilizing particle image veloci- metry, hot-wire anemometer and infrared camera was carried out. The results show that: (1) At the jet orifice exit, pairs of vortexes are generated, broken down and merged together periodically, forming a steady jet within a several slot width from distance near the orifice exit. And during the development, the synthetic jet spreads rapidly along the minor axis direction of the orifice. While along the major axis direction, the synthetic jet contracts firstly and then spreads slowly. (2) Exci- tation frequency forced on the actuator has a great effect on the synthetic jet flow field. There are two resonance frequencies at which the mean velocity and vorticity of the synthetic jet are maximized, especially at the higher resonance frequency. The resonance frequency values obtained by the experiment are lower than the theoretical values. (3) Similarly to the common jet impingement, the convective heat transfer coefficients at the target surface impinged by the synthetic jet also take on up-down tendency varying with the jet-to-surface spacing increment. But the jet-to-surface spacing ratio for optimum cooling achievement is greater and the cooling action region is wider than the former, indicating that the synthetic jet in- troduces a stronger entrainment and more vigorous penetration in the surrounding fluid. To investigate the flow and heat transfer characteristics of a synthetic jet driven by piezoelectric actuator, experimental investigation utilizing particle image velocimetry, hot-wire anemometer and infrared camera was carried out. The results show that: (1) At the jet orifice exit, pairs of vortexes are generated, broken down and merged together periodically, forming a steady jet within a several slot width from distance near the orifice exit. And during the development, the synthetic jet spreads rapidly along the minor axis direction of the orifice. While along the major axis direction, the synthetic jet contracts firstly and then spreads slowly. (2) Excitation frequency forced on the actuator has a great effect on the synthetic jet flow field. There are two resonance frequencies at which the mean velocity and vorticity of the synthetic jet are maximized, especially at the higher resonance frequency. The resonance frequency values obtained by the experiment are lower than the theoretical values. (3) Similarly to the common jet impingement, the convective heat transfer coefficients at the target surface impinged by the synthetic jet also take on up-down tendency varying with the jet-to-surface spacing increment. But the jet-to-surface spacing ratio for optimum cooling achievement is greater and the cooling action region is wider than the former, indicating that the synthetic jet introduces a stronger entrainment and more vigorous penetration in the surrounding fluid.
出处 《Science China(Technological Sciences)》 SCIE EI CAS 2007年第2期221-229,共9页 中国科学(技术科学英文版)
基金 Supported by the National Natural Science Foundation of China (Grant No. 50276028)
关键词 SYNTHETIC JET IMPINGING COOLING flow HEAT TRANSFER synthetic jet impinging cooling flow heat transfer
  • 相关文献

参考文献2

二级参考文献19

  • 1[1]Hassan A A, Domzalski D B, JanakiRam R D, et al. Prospects of using zero- mass synthetic jets for improved helicopter/tiltrotor aerodynamic performance [A]. Annual Forum Proceedings [C]. American Helicopter Society, 1998, (1):511- 526.
  • 2[2]Hassan A A, Jankira R D, Effects of zero- mass synthetic jet on the aerodynamics of the NACA- 0012 airfoil [J]. Journal of the American Helicopter Society, 1998, 43 (4): 303- 311.
  • 3[3]Smith Douglas R, Kibens Valdis, Pitt Dale M, et al. Effect of synthetic jet arrays on boundary layer control [A]. Proceedings of SPIE [C]. The International Society for Optical Engineering, 1999, (3674):401- 409.
  • 4[4]Coe D J, Allen M G, Smith B L, et al. Addressable micromachined jet arrays [A]. International Conference on Solid- State Sensors and Actuators, and Eurosensors IX, Proceedings 2 IEEE [C]. 1995:329- 332.
  • 5[5]Campbell J, Stephen Jr, Black W Z, et al . Thermal management of a laptop computer with synthetic air microjets [A]. Thermal mechanical phenomena in electrical systems- proceedings of the intersociety conference, IEEE [C]. 1998:43- 50.
  • 6[6]Smith B L, Glezer A. The formation and evolution of synthetic jets [J]. Phys Fluids, 1998, 10(9): 2281- 2297.
  • 7[7]Rizzetta D P, Visbal M R, Stanek M J. Numerical investigation of synthetic- jet flowfields [J]. AIAA Journal , 1999, 37(8):919- 927.
  • 8Smith B L,Glezer A.The Formation and Evolution of Synthetic Jets[J].Physics of Fluids,1998,10(9):2281~2297.
  • 9Linda D K,John F D.Numerical Simulation of Synthetic Jet Actuators[R].AIAA Paper 97-1924,1997.
  • 10Rizzerta D P,Visbal M R,Stanek M J.Numerical Investigation of Synthetic-Jet Flowfields[J].AIAA Journal,1999,37(8):919~927.

共引文献20

同被引文献55

引证文献9

二级引证文献43

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部