【24h】

CAVITY FLOW IN A BOUNDARY LAYER

机译:边界层中的空腔流动

获取原文

摘要

A numerical-and-analytical method for solving cavity flows in a vortex incidence flow is proposed. The continuous vorticity arbitrary displayed in the flow field is replaced by discrete vortex lines coinciding with stream lines. The flow between these lines is assumed to be vortex free. The problems of the flow in channels formed by stream/vortex lines and the problem of the cavity flow in a jet of a finite width connected to each other by the derived interaction conditions are solved by using complex variable theory. The numerical procedure is based on the method of successive approximations and adopted to investigate the effect of the velocity gradient in a boundary layer on parameters of the cavity flow. The presented calculations show that, at some fixed cavity length, the cavity number and drag coefficient decreases with the increase of the boundary layer width.
机译:提出了一种求解旋涡入射流腔流的数值分析方法。在流场中任意显示的连续涡旋被与流线一致的离散涡旋线代替。这些线之间的流动被假定为无涡流。利用复变理论解决了由流/涡旋线形成的通道中的流动问题和通过导出的相互作用条件相互连接的有限宽度的射流中的腔室流动问题。数值程序是基于逐次逼近的方法,并用于研究边界层中速度梯度对型腔流动参数的影响。计算结果表明,在一定的模腔长度下,模腔数和阻力系数随边界层宽度的增加而减小。

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