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几何参数影响改进型压电合成射流驱动器实验
引用本文:张立,王帮峰,周勇.几何参数影响改进型压电合成射流驱动器实验[J].航空动力学报,2011,26(11):2503-2509.
作者姓名:张立  王帮峰  周勇
作者单位:1. 南京航空航天大学航空宇航学院,南京,210016
2. 南京信息工程大学气象传感网络技术工程中心,南京,210044
基金项目:国家自然科学基金(90405008, 10772081, 90605003)
摘    要:通过实验的方法研究了开孔尺寸与腔体体积对改进型压电合成射流驱动器出口处射流强度的影响,由热线风速仪测得的瞬时速度,得到了各驱动器试件单位周期内最大速度与时均速度的频响曲线,并引入腔体体积与开孔面积的比值作为无量纲参数,使得能够将驱动器几何尺寸参数对其射流的影响统一起来.结果显示:在低 频谐振频率处,单位周期内最大速度值与时均速度值单调下降;而在高频谐振频率处,时均速度单调下降,单位周期内最大速度值存在极值点;驱动器的几何参数主要对高频区的谐振频率有重要影响. 

关 键 词:改进型压电合成射流驱动器    几何参数    热线风速仪    频率响应    时均速度
收稿时间:2010/12/22 0:00:00
修稿时间:2011/3/18 0:00:00

Experimental investigation on improved piezoelectric synthetic jet actuator of geometric parameters
ZHANG Li,WANG Bang-feng and ZHOU Yong.Experimental investigation on improved piezoelectric synthetic jet actuator of geometric parameters[J].Journal of Aerospace Power,2011,26(11):2503-2509.
Authors:ZHANG Li  WANG Bang-feng and ZHOU Yong
Institution:ZHANG Li1,WANG Bang-feng1,ZHOU Yong2 (1.College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China,2.Technology and Engineering Center for Meterological Sensor Network,Nanjing University of Information Science and Technology,Nanjing 210044,China)
Abstract:A novel piezoelectric synthetic jet actuator was studied experimentally.The velocities of outflows were detected by hotwire anemometer.The frequency responses of time-average velocity and maximum velocity during one period were obtained.The results show that:in the region of low frequency,the time-average velocity and maximum velocity decrease monotonically;in the region of high frequency,the maximum velocity is affected by geometric parameters of the actuator evidently.And there is an optimum geometric size for the actuator to obtain the maximum peak velocity during the high frequency region.
Keywords:improved piezoelectric synthetic jet actuator  geometric parameter
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