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Large eddy simulation of unsteady flow past a circular cylinder.

机译:穿过圆柱体的非定常流动的大涡模拟。

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Flow of an incompressible fluid over a two-dimensional circular cylinder is investigated by solving the vorticity/stream-function version of the two-dimensional Navier-Stokes equations using a finite-difference Large Eddy Simulation (LES) method. Three different subgrid scale (SGS) models are tested. They are the classical Smagorinsky model, Yoshizawa's Two-Scale Direct-Interaction Approximation (TSDIA) model and Canuto's algebraic Reynolds stress (ARS) model. The last two models are dynamical SGS models.; There has been one previous effort using LES with the Smagorinsky model to solve high Reynolds number flow past a circular cylinder. This study, however, is the first to use a dynamical SGS model to solve the problem of flow over a bluff body. For the steady approach flow, calculation of lift and drag coefficients at Reynolds numbers of 100, 20,000 and 44,200 compare favorably with available experimental data. The flow fields are shown by vorticity contour plots. A frequency analysis gives more insights to the dynamics of the flow. Overall, our numerical results obtained with the dynamical Yoshizawa model show considerable improvement compared with both the results of the Smagorinsky model carried out in this study and those published in the literature for comparable Reynolds numbers. These results also show that the two-dimensional approach can produce acceptable results for the force acting on the cylinder which, in the case in most engineering applications, is of most interest.; The sinusoidally oscillating flow of {dollar}beta{dollar} = 1035 at Keulegan-Carpenter numbers of 0.4 to 4 are calculated. The instantaneous in-line force coefficient is calculated, then the inertia and drag coefficients of the Morison equation are calculated by a Fourier integration. Vorticity contours are plotted to show that the flow is symmetric for small KC numbers and asymmetric for large KC numbers. A frequency analysis of both the inertia and drag coefficients is carried out to demonstrate the difference between the spectra of small KC numbers and those of large KC numbers. The results for the oscillating flow of small KC numbers agree quite well with Sarpkaya's Morison force coefficient data, as one would expect. But those for large KC numbers are less promising. We conjecture that the two-dimensional approach, even with a good SGS model, is not adequate for the calculations of flows of large KC numbers when the flow is strongly three-dimensional.
机译:通过使用有限差分大涡模拟(LES)方法求解二维Navier-Stokes方程的涡度/流函数形式,研究了不可压缩流体在二维圆柱体上的流动。测试了三种不同的子网格规模(SGS)模型。它们是经典的Smagorinsky模型,Yoshizawa的两尺度直接相互作用逼近(TSDIA)模型和Canuto的代数雷诺应力(ARS)模型。最后两个模型是动态SGS模型。 LES先前曾尝试将LES与Smagorinsky模型一起使用,以解决通过圆柱的高雷诺数流。但是,这项研究是第一个使用动态SGS模型解决在钝体上流动的问题。对于稳定的进场流量,雷诺数分别为100、20,000和44,200时的升力和阻力系数的计算与可用的实验数据相比具有优势。流场由涡度等高线图显示。频率分析可提供有关流动力学的更多见解。总体而言,与本研究中进行的Smagorinsky模型结果和文献中发表的可比较雷诺数的结果相比,通过动力学吉泽模型获得的数值结果显示出相当大的改进。这些结果还表明,二维方法可以对作用在气缸上的力产生可接受的结果,在大多数工程应用中,这是最令人感兴趣的。计算在0.4至4的Keulegan-Carpenter数下,{beta} {{dollar}} = 1035的正弦振荡流。计算瞬时在线力系数,然后通过傅立叶积分计算莫里森方程的惯性和阻力系数。绘制了涡度等高线以显示,对于小KC数,流动是对称的,而对于大KC数,流动是不对称的。进行了惯性系数和阻力系数的频率分析,以证明小KC数和大KC数的频谱之间的差异。正如人们所期望的那样,小KC数振荡流的结果与Sarpkaya的Morison力系数数据非常吻合。但是,对于大量KC而言,前景不太乐观。我们猜想,当流动为强三维时,即使采用良好的SGS模型,二维方法也不足以用于计算大KC数的流动。

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