...
首页> 外文期刊>Journal of Fluids and Structures >Flow behavior around a square cylinder subject to modulation of a planar jet issued from upstream surface
【24h】

Flow behavior around a square cylinder subject to modulation of a planar jet issued from upstream surface

机译:方形圆柱体周围的流动特性受到上游表面发出的平面射流的调节

获取原文
获取原文并翻译 | 示例

摘要

The flow behavior in the up- and downstream regions of a square cylinder subject to the modulation of a planar jet issued from the cylinder's front surface was studied using the laser-assisted smoke flow visualization method and hot-wire anemometer measurement. Reynolds numbers were from 1628 to 13 000. The drag force experienced by the square cylinder was obtained by measuring the surface pressures on the up- and downstream faces. The temporally evolving smoke flow patterns in the up- and downstream regions were synchronously revealed through the smoke flow visualization. The frequency characteristics of the instability waves in the up- and downstream regions were synchronously detected by the two hot-wire anemometers. Four characteristic flow modes were observed within the different ranges of the injection ratios. At the low injection ratios (IR < 1), the 'swinging jet' appeared. The jet swung periodically leftward and rightward and formed a fluid bubble on the front surface. The fluid bubble contained a pair of counter-rotating vortices and presented a periodic variation in its height. At moderately low injection ratios (1 < IR < 4.3), the 'deflected oscillating jet' appeared. The jet was deflected in either the left or the right direction and wrapped around one of the edges of the square cylinder. Both the swinging and oscillating motions of the jet in the swinging jet and deflected oscillating jet modes were induced by the periodic feedback pressure signals generated by the vortex shedding in the wake. At the moderately high (4.3 < IR < 8.3) and high (IR > 8.3) injection ratios, the 'deflection jet' and 'penetrating jet' appeared. The jet detached from the cylinder's front surface and penetrated a long distance into the upstream region due to large jet momentum. Neither periodic jet oscillation in the upstream region nor vortex shedding in the wake was observed. The drag coefficient was found to be decreasing quickly with increasing the injection ratio. (C) 2014 Elsevier Ltd. All rights reserved.
机译:使用激光辅助烟流可视化方法和热线风速仪测量研究了方形圆柱体上下区域中的流动行为,该流动行为受到圆柱前表面发出的平面射流的调制。雷诺数为1628至13000。通过测量上,下游面上的表面压力来获得方形圆柱体承受的阻力。通过烟流可视化同步显示了上下游区域随时间变化的烟流模式。通过两个热线风速仪同步检测上下区域不稳定波的频率特性。在喷射比的不同范围内观察到四个特征流动模式。在低喷射比(IR <1)下,出现了“摆动射流”。射流周期性地左右摆动,并在前表面形成气泡。气泡包含一对反向旋转的涡流,并且高度呈周期性变化。在中等较低的喷射比(1 8.3)下,出现了“偏转射流”和“穿透射流”。由于大的射流动量,射流从气缸的前表面脱离,并很长一段距离进入上游区域。既没有观察到上游区域的周期性射流振荡,也没有观察到尾流中的涡旋脱落。发现阻力系数随着注射比的增加而迅速减小。 (C)2014 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号