Bulletin of the American Physical Society
71st Annual Meeting of the APS Division of Fluid Dynamics
Volume 63, Number 13
Sunday–Tuesday, November 18–20, 2018; Atlanta, Georgia
Session G21: Boundary Layer Flows over Rough Surfaces I |
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Chair: Michael Benson, US Military Academy Room: Georgia World Congress Center B309 |
Monday, November 19, 2018 10:35AM - 10:48AM |
G21.00001: Direct numerical simulation of turbulent forced convection with roughness Michael MacDonald, Nicholas Hutchins, Daniel Chung We present direct numerical simulations of turbulent forced convection over explicitly gridded three-dimensional sinusoidal roughness. The minimal channel is used to circumvent the high cost of simulating high Reynolds number flows, in which only the near-wall flow is captured. As the roughness Reynolds number, k+, is increased, the Hama roughness function, ΔU+, tends towards the fully rough asymptote which scales with the logarithm of k+. In this fully rough regime, the skin-friction coefficient is constant with bulk Reynolds number, Reb. Meanwhile, the temperature difference between smooth- and rough-wall flows, ΔΘ+, appears to tend towards a constant value. This corresponds to the Stanton number (the temperature analogue of the skin-friction coefficient) monotonically decreasing with Reb in the fully rough regime. While Reynolds analogy, or similarity between momentum and heat transfer, breaks down for the bulk skin-friction and heat-transfer coefficients, similar distribution patterns between the heat flux and viscous component of the wall shear stress is observed. Instantaneous visualizations of the temperature field show a thin thermal diffusive sublayer following the roughness geometry in the fully rough regime, resembling the viscous sublayer of a contorted smooth wall. |
Monday, November 19, 2018 10:48AM - 11:01AM |
G21.00002: Wall-Roughness Eddy Viscosity for Reynolds-Averaged Closures Giles Brereton, Junlin Yuan An approach to modeling the effect of rough surfaces on turbulent boundary-layer flow is presented. It is based on the concept of a rough-wall eddy viscosity, in which the pressure and viscous drag forces which arise on account of flow past roughness elements are recast as an equivalent viscous shear force |
Monday, November 19, 2018 11:01AM - 11:14AM |
G21.00003: Direct Numerical Simulation of Turbulent Flow over Random Roughness Rong Ma, Karim Alame, Krishnan Mahesh Direct numerical simulations (DNS) are performed to study the effects of a random rough wall on turbulent channel flow at $Re_{\tau}=400$ and $Re_{\tau}=600$. The surface geometry matches the experiments of Flack and Schultz (private communication). The skin friction coefficient of the DNS shows good agreement with the experimental results. The mean velocity profiles and velocity fluctuations are compared to smooth channel flow. Pressure fluctuations are more intense in the roughness layer. The mean momentum budget is examined. It is seen that roughness causes the transition from viscous to inertial dominance to occur closer to the wall compared to a smooth wall. |
Monday, November 19, 2018 11:14AM - 11:27AM |
G21.00004: Comparison of LES and measurements of flow over rough surfaces Vladimír Fuka, Klára Jurčáková, Radka Kellnerová This paper presents simulations of turbulent flow over rough rough surfaces in a wind tunnel. |
Monday, November 19, 2018 11:27AM - 11:40AM |
G21.00005: Turbulence structures in rotating channel flows with rough wall Ugo Piomelli, Wen Wu, Junlin Yuan We performed direct simulations of channel flow subjected to rotation about a spanwise axis, comparing smooth walls and cases with random roughness. Three rotation rates were considered: Ro=0, 0.42 and 1.00; in the last case the flow becomes nearly laminar on the cyclonic, stable, side when the wall is smooth. The destabilizing effect of roughness counteracts the stabilizing effect of rotation, maintaining non-zero Reynolds shear stress at all rotation rates considered. The wake fluctuations result in significant dispersive stresses, which are attenuated by rotation on the cyclonic side. The wake production, however, is small compared to the production term caused by the Coriolis force and the pressure work. The increased pressure fluctuations due to the blockage caused by roughness may be more important, in this flow, than the wake production. The instantaneous fields and spectra highlight the presence of elongated roll cells, which are not sensitive to the roughness. The sweeps and ejections responsible for a significant percentage of the Reynolds stress are due to motion whose coherence, in the wall normal direction, is increased, perhaps due to the effect of the roll cells. |
Monday, November 19, 2018 11:40AM - 11:53AM |
G21.00006: Direct numerical simulations of Taylor-Couette turbulence: dynamics of the fully rough regime Pieter Berghout, Xiaojue Zhu, Daniel Chung, Roberto Verzicco, Richard Stevens, Detlef Lohse Due to its abundance in nature and industry, the study of turbulent flows over rough surfaces is of paramount importance. The key question is how any rough geometry maps to its fluid dynamic behavior. However, the study of open systems is hampered by accurate measurements of the skin-friction drag and the presence of very long spatial structures. In this research, we employ Direct Numerical Simulations (DNSs) of a closed system, Taylor-Couette flow. Whereas before we have focused on transitionally rough surfaces, here we focus on the local and global fluid flow response over fully rough surfaces. In particular we study the azimuthal (streamwise) velocity and angular velocity profiles for varying friction Reynolds number and constant viscous roughness heights. |
Monday, November 19, 2018 11:53AM - 12:06PM |
G21.00007: A stochastic approach to predict flow properties over irregular rough walls Federico Bernardoni, Umberto Ciri, Maria Vittoria Salvetti, Stefano Leonardi The influence of complex terrain orography on the aerodynamic flow field is important in a wide range of applications, from meteorology to wind energy. At the present state of art, it is mainly modeled through some aerodynamic quantities, such as the overall drag coefficient, the roughness length or the roughness function. The aim of this study is to compute with an efficient method the aerodynamic quantities characterizing a irregular rough surface by using a stochastic surrogate model that relies on high fidelity data obtained from DNS. The geometrical parameters of the roughness are treated as uncertain to build a response model in the parameter space of the quantities of interest through the polynomial chaos expansion. Then, a irregular roughness can be described in terms of probability density function of its geometrical parameters and the aerodynamic properties can be obtained by using the stochastic surrogate model together with an efficient sampling of the parameter space based on the Latin Hypercube Sampling method. The need of carrying out computationally expensive wall resolved numerical simulations is avoided in this way. The predictions obtained with the proposed approach are compared against DNS of different irregular rough surfaces showing good agreement. |
Monday, November 19, 2018 12:06PM - 12:19PM |
G21.00008: Rough wall turbulent boundary layers at high packing densities Haosen Xu, Xiang Yang We study rough wall turbulent boundary layers at high surface coverage densities (SCD). We conduct wall-modeled large eddy simulations (WMLES) of flow over aligned cube arrays at surface SCD from 0.4 to 0.9, where the cubes are resolved using an immerse boundary method. The mean flow shows a small velocity deficit at high SCDs, and the flow “slip” over the roughness elements. In addition, two peaks are found in the uu profile at SCD=0.6, where u is the streamwise velocity fluctuation. We show this two-peak behavior is the result of a competition between the Reynolds stress above the roughness-occupied layer and the dispersive stress within the roughness-occupied layer. We will also present evidence from direct numerical simulation (DNS) for the reduced velocity deficit in the mean flow and the two peaks in the turbulent stress profile. |
Monday, November 19, 2018 12:19PM - 12:32PM |
G21.00009: Simulations and experiments of boundary layer flow over a fully rough wall Mary L Houston, Michael Heisel, Michele Guala, Joseph W. Nichols We investigate the effects of three-dimensional roughness on turbulence in the logarithmic layer using direct numerical simulation (DNS) and wind tunnel experiments. The DNS apply an immersed boundary method to model flow over an arbitrarily complicated rough wall boundary. As the simulations progress, an adaptive mesh refinement (AMR) scheme updates the mesh dynamically to resolve small details of the flow along the wall and in areas of high vorticity. We use the simulations to identify coherent structures in the logarithmic layer. Size, size distribution and spatial organization of vortices are studied, as well as the presence of zones of uniform momentum (UMZs) and the associated internal shear layers. The simulations are complemented by wind tunnel experiments at a matched roughness geometry and friction Reynolds number Reτ. We compare the numerical and experimental results as a means to validate the numerical methods. |
Monday, November 19, 2018 12:32PM - 12:45PM |
G21.00010: Investigation of secondary flows in turbulent pipe flows with three-dimensional sinusoidal walls Leon Chan, Michael C MacDonald, Daniel Chung, Nicholas Hutchins, Andrew Ooi The occurrence of secondary flows is systematically investigated via Direct Numerical Simulations (DNSs) of turbulent flow in a rough wall pipe at friction Reynolds numbers of 540. In this study, the peak-to-trough height of the roughness elements, which consist of three-dimensional sinusoidal roughness, is fixed at 120 viscous units while the wavelength of the roughness elements is varied. The solidity or effective slope (ES) of the roughness ranges from the sparse regime (ES = 0.18 with a viscous roughness wavelength, λ+ of 848) to the closely packed roughness/dense regime (ES = 0.72, λ+ = 212). The time-independent dispersive stresses, which arise due to the stationary features of the flow, are analysed and are found to increase with increasing roughness wavelength. These dispersive stresses are related to the occurrence of secondary flows and are maximum within the roughness canopy. Above the crest of the roughness elements, the dispersive stresses reduce to zero at wall-normal heights greater than half of the roughness wavelength. This study has found that the size and wall-normal extent of the secondary flows scales with the roughness wavelength and can reach wall-normal heights of almost half of the pipe radius. |
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