首页> 外文期刊>Wind & structures >Wind-tunnel blockage effect on drag coefficient of circular cylinders
【24h】

Wind-tunnel blockage effect on drag coefficient of circular cylinders

机译:风洞阻塞对圆柱体阻力系数的影响

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

This paper explains how to correctly measure the drag coefficient of a circular cylinder in wind tunnels with large blockage ratios and for the sub-critical to the super-critical flow regimes. When dealing with large blockage ratios, the drag has to be corrected for wall constraints. Different formulations for correcting blockage effect are compared for each flow regime based on drag measurements of smooth circular cylinders performed in a wind tunnel for three different blockage ratios. None of the correction model known in the literature is valid for all the flow regimes. To optimize the correction and reduce the scatter of the results, different correction models should be combined depending on the flow regime. In the sub-critical regime, the best results are obtained using Allen and Vincenti's formula or Maskell's theory with ε=0.96. In the super-critical regime, one should prefer using Glauert's formula with G = 0.6 or the model of Modi and El-Sherbiny. The change in the formulations appears at the flow transition with a variation of the wake pattern when passing from sub-critical to super-critical flow regimes. This parameter being not considered in the known blockage corrections, these theories are not valid for all the flow regimes.
机译:本文介绍了如何正确测量大阻滞比以及次临界至超临界流态下风洞中圆柱的阻力系数。当处理较大的堵塞率时,必须针对壁约束来校正阻力。基于在三种不同的堵塞率下在风洞中进行的光滑圆柱体的阻力测量,针对每种流动状态对用于纠正堵塞效果的不同配方进行了比较。文献中已知的校正模型均不适用于所有流动状态。为了优化校正并减少结果的分散性,应根据流态组合不同的校正模型。在亚临界状态下,使用Allen和Vincenti公式或ε= 0.96的Maskell理论可获得最佳结果。在超临界状态下,应首选使用G = 0.6的Glauert公式或Modi和El-Sherbiny模型。当从亚临界流态转变为超临界流态时,配方的变化出现在流动过渡时,尾流模式发生变化。在已知的堵塞校正中未考虑该参数,这些理论不适用于所有流动状态。

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