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Study of high temperature thermal boundary conditions on active surfaces of the cylinder shaped ultrasonic transducers

机译:圆柱型超声换能器有效表面高温高温边界条件的研究

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Results of an experimental and numerical research of two-dimensional unsteady flow around the butt end of the model of cylinder shaped ultrasonic transducer at zero angle attack are presented. The flow formed employing linear dc plasma torch, is turbulent with Re number between 1.8 x 10~4 and 2.2 x 10~4 and temperature -1200 K. At this regime the flows boundary layers at the cylinder edge separate laminar and transition takes place in the free shear layers. In the shear layer strong vortex shedding and temperature fluctuations are observed. Experimentally estimated distribution of velocities and temperatures on the flat surface of circular cylinder compared with the predicted and has been established good agreement under the results. The influence of the location to distribution and quantity of dynamic and thermal parameters was investigated.
机译:给出了在超声角为零的情况下,圆柱超声换能器模型两端的二维非定常流动的实验和数值研究结果。使用线性直流等离子炬形成的流是湍流的,Re数在1.8 x 10〜4和2.2 x 10〜4之间,温度为-1200K。在这种状态下,圆柱边缘的流边界层分开层流,并在自由剪切层。在剪切层中观察到强烈的涡旋脱落和温度波动。通过实验估算出的圆柱体平面上的速度和温度分布与预测值相比较,并在结果上建立了良好的一致性。研究了位置对动态和热参数分布和数量的影响。

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