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首页> 外文期刊>Journal of Fluid Mechanics >Distorted turbulence and secondary flow near right-angled plates
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Distorted turbulence and secondary flow near right-angled plates

机译:直角板附近的紊流和二次流

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摘要

In many turbulent flows near obstacles or in ducts, the turbulence is inhomogeneous in two directions perpendicular to the main flow direction. In convective flows, there may initially be no mean motion. In both types of flow the gradients of Reynolds stresses drive mean motions in directions of inhomogeneity. Using the method of rapid distortion theory developed by Hunt & Graham (J. Fluid Mech., vol. 84, 1978, p. 209), we analyse these gradients where homogeneous isotropic turbulence is impinging onto two semi-infinite flat rigid surfaces intersecting at right angles. The mean velocity is assumed to be uniform (i.e. the surfaces move at free-stream velocity, or the boundary layers are very thin). The inhomogeneous spectra, variances and Reynolds-stress gradients are evaluated. For isotropic free-stream turbulence with mean square velocity u2∞1?, the mean square velocity fluctuation at a high Reynolds number in the corner is u~2_(∞1?)(X, 0, 0) = 2.121u~2_(∞1?), independent of the form of the spectrum. This is explained by estimating how the free-stream eddies are blocked by the two walls. The gradients of Reynolds stresses force a mean secondary flow to develop; its direction is into the corner, and its magnitude at time t is of order tu~2_(∞1?)/L_∞, where L∞ is the integral scale. These results are tested in a wind tunnel experiment. A turbulence-generating grid installed at the entrance to the test section generates nearly isotropic, grid-generated turbulence. A corner plate with faces parallel to the mean flow and sharp edges is placed downstream of the grid so that shear-free turbulence impinges onto the corner plate. The turbulent Reynolds number based on (L_∞), (Re_L=u ~2_(∞1?)L_∞/v, is 1400 at the leading edge of the plate. A hot-wire anemometry is used to measure instantaneous velocities. The experimental results are consistent with the rapid distortion theory estimates for the variances and the secondary mean motion, which is in the same direction and has the same order of magnitude as Prandtl's analysis of shear-driven secondary flow (of the second kind). We conclude that the blocking mechanism adds to the shear effects and has a significant and sometimes dominant contribution to the crossflows wherever it acts in two non-parallel directions, such as convection in a corner. Consequently, mean transport into corners occurs for most kinds of distorted flow with weak viscous stresses, which has many engineering and environmental implications. There are also implications for the chaotic nature of many confined flows near corners.
机译:在障碍物附近或管道中的许多湍流中,湍流在垂直于主流方向的两个方向上是不均匀的。在对流中,最初可能没有平均运动。在两种类型的流动中,雷诺应力的梯度都会在非均匀性方向上驱动平均运动。使用由Hunt&Graham(J. Fluid Mech。,vol。84,1978,p。209)开发的快速变形理论方法,我们分析了这些均质各向同性湍流撞击到两个相交于半无限平面刚性平面的梯度。直角。假定平均速度是均匀的(即,表面以自由流速度移动,或者边界层非常薄)。评估不均匀光谱,方差和雷诺应力梯度。对于均方速度为u2∞1?的各向同性自由流湍流,拐角处高雷诺数时的方均速度波动为u〜2_(∞1?)(X,0,0)= 2.121u〜2_( ∞1?),与频谱形式无关。通过估计自由流涡流如何被两个壁阻挡来解释这一点。雷诺应力的梯度迫使平均二次流发展;它的方向是角,并且在时间t处的大小为tu〜2_(∞1?)/L_∞,其中L∞是积分标度。这些结果在风洞实验中进行了测试。安装在测试部分入口处的产生湍流的格栅会产生几乎各向同性的,由格栅产生的湍流。将具有平行于平均流量且具有锋利边缘的面的角板放置在网格的下游,以便将无剪切湍流撞击到角板上。基于(L_∞)的湍流雷诺数(Re_L = u〜2_(∞1?)L_∞/ v在板的前沿为1400。热线风速仪用于测量瞬时速度。实验结果与关于方差和二次平均运动的快速失真理论估计相一致,方向和二次平均运动与Prandtl对剪切驱动的二次流(第二类)的分析方向相同,幅度相同。阻塞机制会增加剪切效果,并且无论在两个不平行的方向(例如,对角中的对流)中作用于何处,都对错流产生重大且有时是主要的贡献,因此,对于大多数扭曲流,均会发生向拐角的平均传输粘性应力弱,这对工程和环境都有很多影响,而且对拐角附近许多受限流动的混沌性质也有影响。

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