热边界层湍流流动特性的研究

K. Dennis, K. Siddiqui
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摘要

众所周知,边界层在许多工程系统中起着关键作用。在这些系统中发现的流体动力边界层通常是湍流性质的,并且涉及到传热,由于浮力的影响,进一步增加了流动的复杂性。紊流边界层的组成层之一,即内层,已被确定为可受浮力影响的关键动力紊流现象的所在地。在混合对流流态中,流动惯量和浮力在同一数量级。在这种情况下,从壁面上升的浮力热与惯性驱动的湍流流场相互作用,导致高度复杂的三维流动动力学。过去对该流型的研究大多是计算性的,很少有实验工作。目前对混合对流流态中浮力和流动惯量的相对贡献对湍流现象的影响的认识非常有限。本文对加热光滑水平平板上的混合对流湍流边界层湍流流动现象进行了研究。实验在湍流边界层从下加热的闭环风洞中进行。采用多平面粒子图像测速(PIV)技术捕获了两个平面上相对于流动方向的二维速度场。在理查德森数(Ri)介于0.0和2.0之间的范围内进行实验,以控制浮力相对于流动惯量的相对贡献。利用实测速度场描述了浮力对三维湍流边界层流动的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Investigation of Turbulent Flow Behavior in a Heated Boundary Layer
The boundary layers are known to play key roles in many engineering systems. The hydrodynamic boundary layer found in these systems is often turbulent in nature and heat transfer is involved which further increases flow complexity due to the influence of buoyancy. One of the constituent layers of the turbulent boundary layer, the inner layer, has been established as home to key dynamical turbulent phenomena which can be influenced by the buoyant force. In the mixed convection flow regime, flow inertia and buoyant force are on the same order of magnitude. In this regime, buoyant thermals rising from the wall interact with the inertia-driven turbulent flow field resulting in highly complex three-dimensional flow dynamics. Past research studies conducted in this flow regime have been mostly computational in nature with little experimental work. The current knowledge on the impact of the relative contributions by the buoyant force and flow inertia on turbulent phenomena in the mixed convection flow regime is very limited. This study reports on an investigation into the turbulent flow phenomena present in mixed convection turbulent boundary layer flow over a heated smooth horizontal flat plate. Experiments were performed in a closed loop wind tunnel where the turbulent boundary layer was heated from below. The multi-plane particle image velocimetry (PIV) technique was used to capture two-dimensional velocity fields over two planes with respect to the flow direction. Experiments were conducted over a range of Richardson numbers (Ri) between 0.0 and 2.0 to control the relative contribution of the buoyant force with respect to flow inertia. The measured velocity fields are used to describe the influence of buoyancy on the three-dimensional turbulent boundary layer flow.
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