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Experimental investigation of convective heat transfer on a flat plate subjected to a transversely synthetic jet

机译:横向合成射流在平板上对流传热的实验研究

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In this study, the effect of a synthetic jet on the heat transfer of flow over a flat plate is investigated experimentally. The experimental study is consist of a heater made of copper plate having constant heat flux located in the wind tunnel, and including a synthetic jet actuator injected into the stream by the entrance of plate. The synthetic jet is created by a piston-cylinder mechanism. In the investigations, the Reynolds number in the main stream, the frequency and amplitude of the actuator are changed while the geometry and Prandtl number remain constant for all cases and the effect of these parameters on the convective heat transfer is analyzed. The experiments are carried out at six different frequencies and four different amplitudes. To explain the heat transfer mechanism, the flow visualization is performed by using the smoke-wire method, and the instantaneous flow images are obtained. The experimental results reveal that there is a disruptive effect on the hydrodynamic boundary layer of the synthetic jet actuator. The obtained results are given as dimensionless parameters. It is observed that, the cycle-averaged Nusselt number increases with the increase of both Womersley number(Wo)and dimensionless amplitude(Ao).
机译:在这项研究中,实验研究了合成射流对平板上流动的热传递的影响。实验研究包括一个由铜板制成的加热器,该铜板在风洞中具有恒定的热通量,并且包括一个通过板的入口注入到流中的合成射流致动器。合成射流是通过活塞缸机构产生的。在研究中,改变了主流中的雷诺数,致动器的频率和振幅,同时在所有情况下几何形状和普朗特数均保持不变,并分析了这些参数对对流换热的影响。实验是在六个不同的频率和四个不同的振幅下进行的。为了解释传热机理,使用烟丝法进行了流动可视化,并获得了瞬时流动图像。实验结果表明,对合成射流致动器的流体动力边界层有破坏作用。获得的结果作为无量纲参数给出。观察到,周期平均努塞尔特数随沃默斯利数(Wo)和无量纲振幅(Ao)的增加而增加。

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