...
首页> 外文期刊>Aircraft engineering >Flow characteristics of two-dimensional synthetic jets under diaphragm resonance excitation
【24h】

Flow characteristics of two-dimensional synthetic jets under diaphragm resonance excitation

机译:膜片共振激励下二维合成射流的流动特性

获取原文
获取原文并翻译 | 示例
           

摘要

Purpose This paper aims to experimentally study the external flow characteristic of an isolated two-dimensional synthetic jet actuator undergoing diaphragm resonance.Design/methodology/approach The resonance frequency of the diaphragm (40 Hz) depends on the excitation mechanism in the actuator, whereas it is independent of cavity geometry, excitation waveform and excitation voltage. The velocity response of the synthetic jet is influenced by excitation voltage rather than excitation waveform. Thus, this investigation selected four different voltages (5, 10, 15 and 20 V) under the same sine waveform as experiment parameters.Findings The velocity field along the downstream direction is classified into five regions, which can be obtained by hot-wire measurement. The first region refers to an area in which flow moves from within the cavity to the exit of orifice through the oscillation of the diaphragm, but prior to the formation of the vortex of a synthetic jet. In this region, two characteristic frequencies exist at 20 and 40 Hz in the flow field. The second region refers to the area in which the vortices of a synthetic jet fully develop following their initial formation. In this region, the characteristic frequencies at 20 and 40 Hz still occur in the flow field. The third region refers to the area in which both fully developed vortices continue traveling downstream. It is difficult to obtain the characteristic frequency in this flow field, because the mean center velocities (umacron) decay downstream and are proportional to (x/w)(-1/2) for the four excitation voltages. The fourth region reveals variations in both vortices as they merge into a single vortex. The mean center velocities (umacron) are approximately proportional to (x/w)(0) in this region for the four excitation voltages. A fifth region deals with variations in the vortex of a synthetic jet after both vortices merge into one, in which the mean center velocities (umacron) are approximately proportional to (x/w)(-1) in this region for the four excitation voltages (x/w is the dimensionless streamwise distance).Originality/value Although the flow characteristics of synthetic jets had reported for flow control in some literatures, variations of flow structure for synthetic jets are still not studied under the excitation of diaphragm resonance. This paper showed some novel results that our velocity response results obtained by hot-wire measurement along the downstream direction compared with flow visualization resulted in the classification of five regions under the excitation of diaphragm resonance. In the future, it makes valuable contributions for experimental findings to provide researchers with further development of flow control.
机译:目的本文旨在通过实验研究隔离的二维合成射流致动器在膜片共振下的外部流动特性。设计/方法/方法膜片的共振频率(40 Hz)取决于致动器中的激励机制,而它与腔的几何形状,激励波形和激励电压无关。合成射流的速度响应受激励电压而不是激励波形的影响。因此,本研究在相同的正弦波形下选择了四个不同的电压(5、10、15和20 V)作为实验参数。发现沿下游方向的速度场分为五个区域,可通过热线测量获得。第一区域是指这样的区域,在该区域中,流体通过膜片的振动从腔内移动到孔口的出口,但是在合成射流的旋涡形成之前。在该区域中,流场中存在20 Hz和40 Hz的两个特征频率。第二区域是指合成射流的涡流在初始形成后完全展开的区域。在该区域中,流场中仍会出现20和40 Hz的特征频率。第三区域是两个完全发展的涡流继续向下游传播的区域。在此流场中很难获得特征频率,因为平均中心速度()向下游衰减,并且与四个激励电压成正比(x / w)(-1/2)。第四区域揭示了两个涡旋合并为一个涡旋时的变化。对于四个激励电压,在该区域中的平均中心速度()大约与(x / w)(0)成比例。在两个涡流合并为一个后,第五个区域处理合成射流的涡流变化,其中四个区域的平均中心速度()均与该区域的(x / w)(-1)成正比。原始电压值尽管一些文献报道了合成射流的流动特性用于流量控制,但在膜片共振激发下仍未研究合成射流的流动结构变化。本文显示了一些新颖的结果,即通过沿下游方向进行热线测量而获得的速度响应结果与流动可视化相比,在膜片共振激发下对五个区域进行了分类。将来,它将为实验结果做出宝贵的贡献,为研究人员提供流量控制的进一步发展。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号