首页> 外文期刊>International Journal of Heat and Fluid Flow >Time resolved investigations on flow field and quasi wall shear stress of an impingement configuration with pulsating jets by means of high speed PIV and a surface hot wire array
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Time resolved investigations on flow field and quasi wall shear stress of an impingement configuration with pulsating jets by means of high speed PIV and a surface hot wire array

机译:高速PIV和表面热丝阵列对脉动射流冲击构型的流场和准壁剪应力的时间分辨研究。

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The effects of jet pulsation on flow field and quasi wall shear stress of an impingement configuration were investigated experimentally. The excitation Strouhal number and amplitude were varied as the most influential parameters. A line-array with three submerged air jets, and a confining plate were used. The flow field analysis by means of time resolved particle image velocimetry shows that the controlled excitation can considerably affect the near-field flow of an impinging jet array. These effects are visualized as organization of the coherent flow structures. Augmentation of the Kelvin-Helmholtz vortices in the jet shear layer depends on the Strouhal number and pulsation magnitude and can be associated with pairing of small scale vortices in the jet. A total maximum of vortex strength was observed when exciting with Sr = 0.82 and coincident high amplitudes.rnTime resolved interaction between impinging vortices and impingement plate boundary layer due to jet excitation was verified by using an array of 5 μm surface hot wires. Corresponding to the global flow field modification due to periodic jet pulsation, the impact of the vortex rings on the wall boundary layer is highly influenced by the above mentioned excitation parameters and reaches a maximum at Sr = 0.82.
机译:实验研究了射流脉动对撞击结构流场和准壁剪切应力的影响。激发斯特劳哈尔数和振幅作为最有影响力的参数而变化。使用具有三个浸没式空气射流的线阵和一个限制板。通过时间分辨粒子图像测速法进行的流场分析表明,受控的激发会显着影响撞击射流阵列的近场流。这些效果可视为相干流动结构的组织。射流剪切层中Kelvin-Helmholtz涡旋的增强取决于Strouhal数和脉动幅度,并且可能与射流中小规模涡旋的配对有关。当使用Sr = 0.82激发并同时出现高振幅时,观察到涡旋强度的总最大值。通过使用5μm表面热线阵列,验证了喷射涡流引起的撞击涡流与撞击板边界层之间的时间分辨相互作用。对应于由于周期性射流脉动而引起的整体流场变化,涡流环对壁边界层的影响受到上述激发参数的强烈影响,并在Sr = 0.82时达到最大值。

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