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Amplitude modulation of streamwise velocity fluctuations in the roughness sublayer: evidence from large-eddy simulations

机译:粗糙度子层中水流速度波动的幅度调制:大涡模拟的证据

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摘要

Recent studies have demonstrated that large- and very-large-scale motions in the logarithmic region of turbulent boundary layers 'amplitude modulate' dynamics of the near-wall region (Marusic et al. Science, vol. 329, 2010, pp. 193-196; Mathis et al., J Fluid Mech., vol. 628, 2009a, pp. 311-337). These contributions prompted development of a predictive model for near-wall dynamics (Mathis et al., I Fluid Merit., vol. 681, 2011, pp. 537-566) that has promising implications for large-eddy simulations of wall turbulence at high Reynolds numbers (owing to the presence of smaller scales as the wall is approached). Existing studies on the existence of amplitude modulation in wall-bounded turbulence have addressed smooth-wall flows, though high Reynolds number rough-wall flows are ubiquitous. Under such conditions, the production of element-scale vortices ablates the viscous wall region and a new near-wall layer emerges: the roughness sublayer. The roughness sublayer depth scales with aggregate roughness element height, h, and is typically 2h similar to 3h. Above the roughness sublayer. Townsend's hypothesis dictates that turbulence in the logarithmic layer is unaffected by the roughness sublayer (beyond its role in setting the friction velocity and thus inducing a deficit in the mean streamwise velocity known as the roughness function). Here, we present large-eddy simulation results of turbulent channel flow over rough walls. We follow the decoupling procedure outlined in Mathis et al. (J. Fluid Mech., vol. 628. 2009a, 311-337) and present evidence that outer-layer dynamics amplitude modulate the roughness sublayer. Below the roughness element height, we report enormous sensitivity to the streamwise-spanwise position at which flow statistics are measured, owing to spatial heterogeneities in the roughness sublayer imparted by roughness elements. For y/h greater than or similar to 1.5 (i.e. above the cubes, but within the roughness sublayer), topography dependence rapidly declines.
机译:最近的研究表明,湍流边界层的对数区域中的大规模和超大规模运动会“幅度调制”近壁区域的动力学(Marusic等,《科学》,第329卷,2010年,第193- 196; Mathis等人,J Fluid Mech。,第628卷,2009a,第311-337页)。这些贡献促使了近壁动力学预测模型的发展(Mathis等人,I Fluid Merit。,第681卷,2011年,第537-566页),该模型对高壁湍流的大涡模拟具有可观的意义。雷诺数(由于靠近壁时存在较小的比例)。尽管高雷诺数粗糙壁流无处不在,但有关壁面湍流中振幅调制存在的现有研究已解决了光滑壁流问题。在这种条件下,元素尺度旋涡的产生消融了粘性壁区域,并出现了一个新的近壁层:粗糙度子层。粗糙度子层深度与总粗糙度元素高度h成正比,通常为2h类似于3h。在粗糙度子层之上。 Townsend的假设表明,对数层中的湍流不受粗糙度子层的影响(除了其在设置摩擦速度方面的作用之外,因此在称为平均粗糙度的平均水流速度中引起不足)。在这里,我们提出了在粗糙壁上湍流通道流动的大涡模拟结果。我们遵循Mathis等人概述的去耦程序。 (J. Fluid Mech。,第628卷,2009a,311-337),并提出了外层动力学振幅调节粗糙度子层的证据。在粗糙度元素高度以下,由于由粗糙度元素赋予的粗糙度子层中的空间异质性,我们报告了对测量流量统计数据的流向跨度位置的巨大敏感性。当y / h大于或等于1.5(即在立方体上方但在粗糙度子层内)时,形貌相关性迅速下降。

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