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CROSSFLOW OVER A POROUS CIRCULAR CYLINDER WITH SURFACE BLOWING: CFD ANALYSIS WITH EXPERIMENTAL VALIDATION

机译:带有表面吹气的多孔圆柱体上的贯流:带有实验验证的CFD分析

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Crossflow over a porous circular cylinder, with uniform blowing at the surface, was investigated experimentally and numerically. Two free stream conditions, Reynolds numbers 4,100 and 6,200, and five dimensionless blowing rate parameters (ratio of surface blowing to free stream velocity), 0.000 to 0.190, were studied experimentally. For simplicity, results for only one Reynolds number and three blowing cases are presented. A low speed wind tunnel was designed and constructed to give time-smoothed average velocities in the range of 61-122 cm/s. The tunnel was calibrated prior to the study. Velocity and pressure profiles were uniform up to 3.81 cm from the walls of the test section. Turbulence intensity, measured at the center of the test section, was 3.0% with an absolute error of 0.5%. Using hot wire anemometry, time-smoothed velocity profiles were measured at several radial and angular positions from the front to the rear stagnation point. The maximum absolute error in the velocity measurements was 12 cm/s and the positional error of the probe was 0.00254 cm. The numerical study employed the finite element method. The flow field was modeled as two-dimensional with half-symmetry. The unsteady, turbulent (k/e) model had 2,160 elements and 2,287 nodes. Convergence and laminar flow was verified. When blowing was present, the numerical solution was found to give excellent agreement with the experiments in the entire flow field. For the no blowing test case, the agreement with the experiments was also excellent up to 20 deg from the rear stagnation point. Flow visualization, using smoke, was used to qualitatively study the large scale secondary flows in the wake region. These results helped explain the poorer agreement for the no blowing test case.
机译:在实验和数值上研究了表面上具有均匀吹塑的多孔圆柱体的交叉流动。实验研究了两个自由流条件,雷诺数4,100和6,200,以及五维吹入率参数(表面吹向的表面比率),0.000至0.190。为简单起见,展示了一个雷诺数和三种吹扫病例的结果。设计并构造了低速风隧道,以提供61-122cm / s范围内的时间平滑的平均速度。在研究之前校准了隧道。速度和压力曲线均均匀距离试验部分壁高达3.81厘米。在试验部分中心测量的湍流强度为3.0%,绝对误差为0.5%。使用热线风化术,在几个径向和角度位置测量时间平滑的速度曲线,从前方到后停滞点测量。速度测量中的最大绝对误差为12cm / s,探针的位置误差为0.00254厘米。数值研究采用了有限元法。流场与半对称为二维建模。不稳定,湍流(K / E)模型具有2,160个元素和2,287个节点。验证了收敛和层流。当存在吹来时,发现数值溶液与整个流场中的实验提供了良好的一致性。对于无吹测试案例,与实验的协议也是从后停滞点的最佳达20°。使用烟雾的流量可视化用于定性地研究唤醒区域中的大型二级流动。这些结果有助于解释不吹的测试案件的较差协议。

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