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

机译:湍流入射流作用下上游腔边缘附近的流动相互作用分析

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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:由浸入湍流入射流中的空腔形成的流动模式是其几何形状与入射流特性之间复杂关系的解决方案。存在许多具有不同形状和尺寸的空腔,这些空腔在某些情况下会产生重要的不利影响,例如减小风的舒适度或由于共振现象而导致的严重结构问题。除了需要减少与腔相关的负面影响外,还可以考虑修改内腔流型的想法,以在湍流自由射流下间接主动控制外部流。因此,不仅从科学的角度而且从实用的角度使腔流的研究成为非常有趣的课题。我们打算将产生的腔流用作主动流控制系统,以使用其内部的吹气和/或吸气系统来管理其外部的湍流边界层。为了研究涡流行为及其在湍流边界层构型上的发生,在LaCLyFA lm的1.4m测试截面湍流边界层风洞中进行了实验设置。根据拟议的目标,建造了一个木腔,其长宽比(L / D)为1(宽,高和长10 cm),并带有用于流动可视化的玻璃墙。另外,在每个垂直壁中,定位有用于流动喷射系统的翼展方向的空气喷射管18。这项研究包括在不同频率(从10Hz到250Hz)下注入和不注入流量的HWA速度测量,每条管道流量为4L / min。在目前的工作中,我们通过在中心线从2mm到顺风24mm处的三个纵向站进行HWA测量,分析了空腔上游边缘附近的流动相互作用。

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