火花型合成射流激励器流动特性及其激励参数数值研究

单勇; 张靖周; 谭晓茗

火花型合成射流激励器流动特性及其激励参数数值研究

南京航空航天大学能源与动力学院,南京 210016

基金项目: 教育部博士点基金(200802871017,20070287040)

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- 被引次数: 0
出版历程
- 收稿日期: 2010-01-26
- 修回日期: 2010-04-01
- 刊出日期: 2011-03-28

Numerical study of the flow characteristics and excitation parameters for the sparkjet actuator

College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China

摘要

摘要: 利用能量方程中的源项模拟电火花能量的输入,数值模拟了火花型合成射流激励器的流场,获得了激励器的能量蓄积、喷射和吸入过程.结果表明:电火花瞬间能量的输入产生了腔体内的高温、高压环境,从而诱发合成射流的形成;在周期性激励下,合成射流在3个周期后稳定,喷口处的速度呈现非正弦的周期性变化,射流喷射过程时间极短,吸入外界环境气体的过程时间较长,与压电式合成射流明显不同;喷口下游周期性出现的涡对强度大、卷吸能力强.在输入能量和腔体体积不变时,喷口速度随激发频率的增加,先增加后减小,存在最佳激发频率.激发频率的增加缩短了腔体内气体的冷却时间,实验时对激发频率的选取要考虑腔体的耐温能力.
- 火花型合成射流激励器 /
- 合成射流 /
- 数值模拟 /
- 流动特性 /
- 激励参数
Abstract: The way of using the source term in energy equation to simulate the input energy of actuator was reasonably compared with the experimental data for the sparkjet actuator.The processing of energy deposition,discharge and recovery of actuator was obtained.The instance energy input can produce the condition of high pressure and temperature in the actuator,inducing the formation of synthetic jet.Under the periodic action,the velocity of synthetic jet on the nozzle is stabilized on a non-sinusoidal law after three periodic times.The characteristic of short discharge time and long recovery time is different from the piezoelectric synthetic jet.The vortices pair at the downstream of nozzle with high intensity has an ability to roll environment air.While the input energy and actuator volume remain unchanged,the velocity at nozzle is enhanced firstly and then decreased with the increase of the excitation frequency.The recovery stage time is shortened with the increase of excitation frequency.So,the choice of excitation frequency is considered in view of the temperature resistance of actuator.
- sparkjet actuator /
- synthetic jet /
- numerical simulation /

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参考文献(19)

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