首页|喷口直径对声激励器输入功率和膜片振动以及合成射流冲击传热的综合影响

喷口直径对声激励器输入功率和膜片振动以及合成射流冲击传热的综合影响

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针对一个由特定型号扬声器和环形激励腔制备的合成射流声激励器,应用激光位移传感器、粒子图像测速仪和红外热像仪等测试方法,进行了声激励器输入功率和膜片振动、合成射流流场和冲击对流传热系列实验研究,以期揭示喷口直径(dc=2~10mm)的综合影响。研究结果表明:恒定输入功率下,膜片在声激励器器件中的振幅相对于单纯扬声器情形存在不同程度的衰减,在小喷口直径和高激励频率下尤为明显;喷口直径为dc=6 mm的合成射流具有最大的喷吹速度、剪切涡量及其冲击对流传热系数。恒定膜片振幅下,小直径喷口合成射流相较于大直径喷口显示出更强的流动和冲击对流传热能力,但其在高激励频率下需要以付出更大的激励器输入功率为代价。声激励合成射流特征速度与激励频率的增加呈现线性增加的趋势,但激励器输入功率随激励频率的增加却呈现出非单调的变化;与单纯扬声器相比,对于小喷口直径的声激励器,对应于最小输入功率的激励频率向低频方向偏移。就本文的声激励合成射流而言,兼顾声激励器功耗和合成射流冲击对流传热特性,适宜的激励频率、喷口直径和无量纲冲击间距分别确定为f=250 Hz、dc=6 mm和H/dc=6~8。
A comprehensive study on the effects of orifice diameter on power consumption and diagram vibration of an acoustic actuator and impingement heat transfer of a synthetic jet
This study focuses on the synthetic jet actuator,composed of a specific acoustic speaker and an annular actuator cavity.A series of experiments have been conducted to explore the overall impacts of orifice diameter(dc ranging from 2 to 10 mm)on various factors,including the input power,diagram vibration of the acoustic actuator,and the flow field and impingement heat transfer of the synthetic jet.We employed a laser displacement sensor,particle image velocimetry,and an infrared thermal imager.Our results indicate that the orifice diameter significantly influences synthetic jet performance.When the input power is constant,the vibration amplitude of the vibrating diaphragm in the acoustic actuator is attenuated with respect to that in the pure acoustic speaker,especially for small-diameter orifices at high excitation frequencies.We found that a synthetic jet generated from a 6 mm orifice produces the highest ejection velocity,shearing vorticity,and impingement heat transfer coefficient.Under the same vibration amplitude of the vibrating diaphragm,a synthetic jet generated from a small-diameter orifice possesses a stronger flow and heat transfer capacity than one created from a large-diameter orifice.However,this comes with a trade-off of requiring more input power to the acoustic actuator,especially at high excitation frequencies.The characteristic velocity of the synthetic jet increased linearly with the excitation frequency.Conversely,the input power of the acoustic actuator exhibited a non-monotonous change with the excitation frequency.With respect to the pure acoustic speaker,the excitation frequency corresponding to the minimum input power shifted toward the lower end of the acoustic actuator attached to a small-diameter orifice cavity.Considering comprehensive factors such as the power consumption of the acoustic actuator and flow and heat transfer characteristics of the synthetic jet,we recommend an excitation frequency f of 250 Hz,an orifice diameter dc of 6 mm,and a dimensionless impinging distance H/dc of 6 for the current synthetic jet.

synthetic jetacoustic actuatororifice diameter effectpower consumptiondiagram vibrationimpingement heat transfer

谭钧文、吕元伟、张靖周、孙文静、张镜洋

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南京航空航天大学能源与动力学院,南京 210016

南京航空航天大学航天学院,南京 210016

南京航空航天大学机械结构力学及控制国家重点实验室,南京 210016

合成射流 声激励器 喷口直径 功耗 膜片振动 冲击传热

2024

中国科学(技术科学)
中国科学院

中国科学(技术科学)

CSTPCD北大核心
影响因子:0.752
ISSN:1674-7259
年,卷(期):2024.54(12)