首页> 外文期刊>International Journal of Heat and Fluid Flow >Prediction of coherent vortices in an impinging jet with unsteady averaging and a simple turbulent model
【24h】

Prediction of coherent vortices in an impinging jet with unsteady averaging and a simple turbulent model

机译:非稳定平均和简单湍流模型对撞击射流中相干涡的预测

获取原文
获取原文并翻译 | 示例
       

摘要

The classical problem of a plane jet impinging on a flat surface is used here as a test to show that it is possible to use URANS and steady boundary conditions to predict coherent structures in the flow field from a simple model with the unsteady time and ensemble averaging of the quantities proposed by Ha Minh. The two-equation model of Myong and Kasagi, where the damping functions have the appropriate asymptotic behaviour near the wall, is used to solve the problem in two dimensions, for a jet located at a distance equal to ten times the nozzle width, using control volumes and second order finite-differences in time and space. It is found that the unsteady averaging approach of Ha Minh is able to reproduce the coherent vortices observed experimentally in the jet. Spectral analysis shows that the coherent part of the numerical solution is compatible with the vorticity dynamics near the nozzle. Overall, computational results show that the presence of coherent mean field components in the solution, if they are predicted, will improve the performance of even a simple eddy-viscosity model.
机译:飞机射流撞击在平面上的经典问题在本文中用作测试,以表明可以使用URANS和稳定边界条件从具有不稳定时间和整体平均的简单模型预测流场中的相干结构Ha Minh建议的数量。 Myong和Kasagi的两方程模型,其中阻尼函数在壁附近具有适当的渐近特性,用于二维控制问题,对于射流位于等于喷嘴宽度十倍的距离处,使用控制体积和时空的二阶有限差分。人们发现,哈明(Ha Minh)的非平稳平均方法能够重现在实验中观察到的相干涡。频谱分析表明,数值解的相干部分与喷嘴附近的涡旋动力学兼容。总体而言,计算结果表明,如果可以预测溶液中相干平均场分量的存在,即使它们是简单的涡流-粘度模型,也可以提高其性能。

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