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

SHAN Yong; ZHANG Jing-zhou; TAN Xiao-ming

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

更新时间：2026-07-07

- Numerical study of the flow characteristics and excitation parameters for the sparkjet actuator
- Vol. 26, Issue 3, (2011)
- 作者机构：
  
  南京航空航天大学能源与动力学院,南京,210016
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2011
- 稿件说明：
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SHAN Yong, ZHANG Jing-zhou, TAN Xiao-ming. Numerical study of the flow characteristics and excitation parameters for the sparkjet actuator[J]. 2011, 26(3).
DOI：

SHAN Yong, ZHANG Jing-zhou, TAN Xiao-ming. Numerical study of the flow characteristics and excitation parameters for the sparkjet actuator[J]. 2011, 26(3). DOI：

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.

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.

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Related Author

CAO Si

LIU Bao-jie

HAN Shao-bing

ZHONG Jing-jun

YAN Hong-ming

REN Jun-xue

LIU Yu

LIAO Yun-fei

Related Institution

National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics

Marine Engineering College, Dalian Maritime University

School of Energy Science and Engineering, Harbin Institute of Technology

School of Astronautics, Beijing University of Aeronautics and Astronautics

Graduate University of Chinese Academy of Sciences

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