首页> 外文会议>ASME Joint US-European Fluids Engineering Division summer meeting;FEDSM2010 >FLOW OF WALL JET NEAR CHANNEL EXIT AT MODERATE REYNOLDS NUMBER
【24h】

FLOW OF WALL JET NEAR CHANNEL EXIT AT MODERATE REYNOLDS NUMBER

机译:中雷诺数附近通道出口的射流流动

获取原文

摘要

The wall jet flow near channel exit at moderate Reynolds Number, emerging from a two-dimensional channel, is examined theoretically in this study. Poiseuille flow conditions are assumed to prevail far upstream from the exit. The problem is solved using the method of matched asymptotic expansions. The small parameter involved in the expansions is the inverse Reynolds number. The flow and stress fields are obtained as composite expansions by matching the flow in the boundary-layer region near the free surface, flow in the outer layer region and the flow in the core region. The fluid is assumed to be Newtonian and it is found that the jet contracts downstream from the channel exit. The influence of inertia on the shape of free surface, the velocity and stress is emphasized and the higher order boundary layer is explored. To leading order, the problem is similar to the case of the free jet (Tillett) [1] with different boundary conditions. A similarity solution can be carried out using a similarity variable problem which is then solved as an initial-value problem, where the equation is integrated subject to the boundary conditions and a guessed value of the slope at the origin. The slope is adjusted until reasonable matching is achieved between the solution and the asymptotic form at large 9. The level of contraction is essentially independent of inertia, but the contraction moves further downstream with increasing Reynolds number. The present work provides the correct conditions near exit, which are required to determine the jet structure further downstream. If the jet becomes thin far downstream, a boundary layer formulation can be used with the presently predicted boundary conditions for steady and possibly transient flows.
机译:在这项研究中,从理论上研究了从二维通道中出来的中等雷诺数通道出口附近的壁面射流。假定Poiseuille流动条件占主导地位,离出口很远。使用匹配渐近展开法可以解决该问题。展开所涉及的小参数是逆雷诺数。通过匹配自由表面附近边界层区域中的流动,外层区域中的流动和核心区域中的流动,将流场和应力场作为复合膨胀获得。假定流体是牛顿流体,并且发现射流在通道出口的下游收缩。强调了惯性对自由表面形状,速度和应力的影响,并探索了高阶边界层。按照领先的顺序,问题类似于具有不同边界条件的自由射流(Tillett)[1]的情况。可以使用相似性变量问题执行相似性解决方案,然后将其作为初始值问题进行求解,在该问题中,方程式受边界条件和原点处的斜率猜测值的影响而积分。调整斜率,直到在9处解和渐近形式之间实现合理匹配为止。收缩水平基本上与惯性无关,但是随着雷诺数的增加,收缩进一步向下游移动。当前的工作提供了在出口附近的正确条件,这是确定更下游射流结构所必需的。如果射流在下游变得稀薄,则可以将边界层公式与当前预测的边界条件一起使用,以实现稳定且可能为瞬态的流动。

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