首页> 外文期刊>Letters in heat and mass transfer >Flow evolution and mass transfer in a turbulent rectangular free jet of air with small laminar Schmidt number
【24h】

Flow evolution and mass transfer in a turbulent rectangular free jet of air with small laminar Schmidt number

机译:小层流Schmidt数的湍流矩形自由射流中的流动演化和传质

获取原文
获取原文并翻译 | 示例
           

摘要

Numerical results are presented for flow evolution, mass transfer and evaluation of the turbulent Schmidt number in a turbulent submerged free jet of air with small laminar Schmidt number (Sc = 0.1). A series of Large Eddy Simulation (LES) are carried on in the Reynolds number range from 5000 to 40,000. The numerical results are reported in terms of instantaneous and mean velocities, static pressure, passive scalar fields and turbulent Schmidt number. The numerical results show that the instantaneous cross-stream velocity and the static pressure are null in the Negligible Disturbance Flow (NDF) and the Small Disturbance Flow (SDF) of the instantaneous jet evolution, allowing a new definition of NDF and SDF. Similarly, the numerical mean static pressure is null in the Undisturbed Region of Flow (URF) of the mean evolution, allowing a new definition of URF. The turbulent Schmidt number shows differences at the two smallest Reynolds numbers, Re = 5000 and 10,000, in comparison to the previous numerical results, obtained with a laminar Schmidt number equal to Sc = 1. A theoretical model is proposed for the passive scalar diffusion in the Undisturbed Region of Flow (URF) and the Potential Core Region (PCR), under the hypotheses of self-similarity, according to the Tollmien and Gortler approaches. The solutions of the present theoretical models, at Sc = 0.1, are self-similar in the PCR and in good agreement with the LES numerical results of the passive scalar, while the passive scalar profiles are not self-similar in the URF at the smaller Reynolds numbers, differently from what happens with a laminar Schmidt number in the range 1-100. The theoretical model assumes a turbulent Schmidt number inversely proportional to the mean velocity gradient in the PCR, as suggested by the LES results. The numerical results of the Sc-T in the URF are variable in the range 0-0.85, which is a value commonly suggested in the literature. In the PCR the values of Sc-T are variable between zero and a maximum which is one order of magnitude greater than in the URF.
机译:给出了数值计算结果,用于在小层流Schmidt数(Sc = 0.1)的湍流浸没式自由射流中的流动演化,传质和湍流Schmidt数的评估。雷诺数范围从5000到40,000,进行了一系列大涡模拟(LES)。以瞬时速度和平均速度,静压力,被动标量场和湍流施密特数表示了数值结果。数值结果表明,瞬时射流演变过程的可忽略扰动流和小扰动流中的瞬时横流速度和静压为零,从而为NDF和SDF提供了新的定义。类似地,数值平均静压力在平均演变的无扰动流动区域(URF)中为零,从而为URF提供了新的定义。与先前的层状Schmidt数等于Sc = 1的数值结果相比,湍流的Schmidt数在两个最小的雷诺数Re = 5000和10,000处显示出差异。为无源标量扩散提出了理论模型根据Tollmien和Gortler方法,在自相似性假设下,流量不受干扰的区域(URF)和潜在核心区域(PCR)。当前理论模型的解在Sc = 0.1时在PCR中是自相似的,并且与无源标量的LES数值结果高度吻合,而在较小的URF中,无源标量分布图不是自相似的雷诺数与层状施密特数在1-100范围内发生的变化不同。理论模型假设湍流的施密特数与PCR中的平均速度梯度成反比,如LES结果所示。 URF中Sc-T的数值结果在0-0.85范围内变化,这是文献中通常建议的值。在PCR中,Sc-T的值在0到最大值之间变化,最大值比URF大1个数量级。

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