...
首页> 外文期刊>Environmental Fluid Mechanics >A simplified computational analysis of turbulent plumes and jets
【24h】

A simplified computational analysis of turbulent plumes and jets

机译:湍流羽流和射流的简化计算分析

获取原文
获取原文并翻译 | 示例

摘要

The application of computational fluid dynamics (CFD), particularly Large Eddy Simulation, for the modelling of buoyant turbulent plumes, has been demonstrated to be very accurate, but computationally expensive. Here a more basic, and therefore more generally practicable, approach is presented. Commercial CFD software is used to model such plumes using Reynolds-Averaged Navier-Stokes (RANS) turbulence models. A careful comparison is made between the numerical predictions and well-established results regarding the bulk properties of plumes. During this process, we are able to observe the well-known approximate Gaussian nature of the plume and achieve quantitative agreement with empirical plume spread coefficients. The use of numerical modelling allows for the investigation of the flow field and turbulence in those regions of the plume of most interest—the plume edge and near source regions. A comprehensive sensitivity study is conducted to identify the limits of applicability of this modelling approach. It is shown that the standard modelling approach of Morton, Taylor and Turner, which introduced the well-known entrainment assumption, pertains in a region well above the source region. At the plume edge, the levels of turbulence are contrasted with the value of the entrainment parameter. Finally, the effects of forcing the plumes with additional momentum at the source are considered, including the case of a pure jet. We show how these forced plumes eventually lose their momentum excess and tend to the behaviour of a pure, buoyant plume.
机译:计算流体动力学(CFD),特别是大涡模拟,用于浮力湍流羽流的建模已被证明是非常准确的,但计算量很大。这里提出了一种更基本,因此更普遍可行的方法。商业CFD软件用于使用雷诺平均Navier-Stokes(RANS)湍流模型对此类羽流建模。在数值预测和关于羽流的总体性质的公认结果之间进行了仔细的比较。在此过程中,我们能够观察到羽流的众所周知的近似高斯性质,并与经验羽流扩散系数达成定量一致。使用数值模型可以研究最感兴趣的羽流区域中的流场和湍流,即羽流边缘和源区域附近。进行了全面的敏感性研究,以确定这种建模方法的适用范围。结果表明,引入众所周知的夹带假设的Morton,Taylor和Turner的标准建模方法适用于远高于源区域的区域。在羽状边缘,湍流水平与夹带参数的值形成对比。最后,考虑了在源头处以附加动量推动羽流的效果,包括纯射流的情况。我们展示了这些强制羽流最终如何失去其多余的动量,并趋向于纯净,漂浮的羽流。

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