首页> 外文会议>AIAA fluid dynamics conference and exhibit >Flow Interaction Analysis Near the Upstream Cavity Edge under Turbulent Incident Flow
【24h】

Flow Interaction Analysis Near the Upstream Cavity Edge under Turbulent Incident Flow

机译:湍流入射流下上游腔边缘附近的流动相互作用分析

获取原文

摘要

The flow pattern developed by a cavity inmersed in a turbulent incident flow is the solution of a complex relation between its geometry and the incident flow characteristics. There are cavities of many different shapes and sizes which in some situations generate important adverse effects such as wind confort reduction or severe structural problems due to resonance phenomena. Besides the need of reducing this negative consequences associated to the cavity, it is possible to think about the idea of modifying the inner cavity flow pattern to make indirect active control over the external flow under turbulent incident free stream. This reasons make the study of cavity flow a very interesting topic not only from a scientific but also from practical point of view. We intend to use the cavity flow generated as an active flow control system to manage the turbulent boundary layer outside it, using a blowing and/or suction system inside it. An experimental setup was made in the LaCLyFA's lm by 1.4m test section turbulent boundary layer wind tunnel, in order to study the vortex behavior and its incidence on the turbulent boundary layer configuration. According to the proposed objectives a wooden cavity was constructed which has an aspect ratio (L/D) of 1 (wide, height and long 10 cm.), with a glass wall for flow visualization. Also, in each vertical wall 18 spanwise air injection tubes for the flow injection system were located. This study consist on HWA velocity measurements with and without flow injection at different frequencies (from 10Hz to 250Hz) for a flow rate of 4L/min per pipe. In the present work we analyse the flow interaction near the upstream edge of the cavity by means of HWA measurements on three longitudinal stations at the centerline starting from 2mm and up to 24mm downwind.
机译:由腔体开发的流动模式在湍流入射流中夹持的是其几何形状和入射流特性之间复杂关系的解决方案。在某些情况下存在许多不同形状和尺寸的腔,这在某些情况下产生了重要的不利影响,例如由于共振现象引起的风中的减少或严重的结构问题。除了需要减少与腔相关的这种负面后果之外,可以考虑改变内腔流动模式的想法,以在湍流入射流下的外部流动下间接主动控制。这一原因使腔体流动的研究不仅来自科学,而且从实际的角度来看。我们打算使用作为主动流量控制系统产生的腔流量来在其内部使用吹气和/或抽吸系统来管理其外部的湍流边界层。在LaClyFA的LM中,在1.4M试验部分湍流边界层风洞中进行了实验设置,以研究涡流行为及其在湍流边界层配置上的发病。根据所提出的目的,构造了木腔,其具有1(宽,高度和长10厘米)的纵横比(L / D),具有用于流动可视化的玻璃壁。而且,在每个垂直壁18中,用于流动喷射系统的始线空气注入管。该研究包括HWA速度测量,在不同频率(10Hz至250Hz)下没有流喷射的流量测量,用于每管4L / min的流速。在本工作中,我们通过从2mm开始的中心线的三个纵向站上的三个纵向站点分析空腔上游边缘附近的流动相互作用。

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