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Resolving turbulence and drag over textured surfaces using texture-less simulations:
the case of slip/no-slip textures

W. Xie \aff1    C. T. Fairhall \aff1    R. García-Mayoral \aff1 \corresp r.gmayoral@eng.cam.ac.uk \aff1Department of Engineering, University of Cambridge, Cambridge, CB2 1PZ, UK
Abstract

We study the effect of surface texture on an overlying turbulent flow for the case of textures made of an alternating slip/no-slip pattern, a common model for superhydrophobic surfaces, but also a particularly simple form of texture. For texture sizes L+25L^{+}\gtrsim 25, we have previously reported that, even though the texture effectively imposes homogeneous slip boundary conditions on the overlying, background turbulence, this is not its sole effect. The effective conditions only produce an origin offset on the background turbulence, which remains otherwise smooth-wall-like. For actual textures, however, as their size increases from L+25L^{+}\gtrsim 25 the flow progressively departs from this smooth-wall-like regime, resulting in additional shear Reynolds stress and increased drag, in a non-homogeneous fashion that could not be reproduced by the effective boundary conditions. This paper focuses on the underlying physical mechanism of this phenomenon. We argue that it is caused by the non-linear interaction of the texture-coherent flow, directly induced by the surface topology, and the background turbulence, as it acts directly on the latter and alters it. This does not occur at the boundary where effective conditions are imposed, but within the overlying flow itself, where the interaction acts as a forcing on the governing equations of the background turbulence, and takes the form of cross-advective terms between the latter and the texture-coherent flow. We show this by conducting simulations where we remove the texture and introduce additional, forcing terms in the Navier-Stokes equations, in addition to the equivalent homogeneous slip boundary conditions. The forcing terms capture the effect of the non-linear interaction on the background turbulence without the need to resolve the surface texture. We show that, when the forcing terms are derived accounting for the amplitude modulation of the texture-coherent flow by the background turbulence, they quantitatively capture the changes in the flow up to texture sizes L+70L^{+}\approx 70100100. This includes not just the roughness function but also the changes in the flow statistics and structure.

keywords:
Near-wall turbulence, surface texture

1 Introduction

This paper focuses on the effect on wall turbulence of surface texture, which alters the flow and modifies the drag compared to a smooth surface. The most common example of surface texture is roughness (Schlichting, 1937; Colebrook & White, 1937; Jiménez, 2004; Chung et al., 2021), which generally increases drag, but there are also textures such as riblets (Walsh & Lindemann, 1984), superhydrophobic surfaces (Rothstein, 2010) and anisotropic permeable substrates (Abderrahaman-Elena & García-Mayoral, 2017; Gómez-de-Segura & García-Mayoral, 2019) that can reduce drag.

According to the classical theory of wall turbulence, for small textures the only effect of the surface on the outer flow is a uniform shift in the mean velocity profile, ΔU+\Delta U^{+}, compared to a smooth surface (Clauser, 1956; Spalart & McLean, 2011; García-Mayoral et al., 2019). The superscript ‘+’ indicates scaling in viscous units, i.e. normalisation by the the kinematic viscosity ν\nu and friction velocity uτ=τwu_{\tau}=\sqrt{\tau_{w}}, where τw\tau_{w} is the tangential stress at the wall. Throughout the paper, we consider upward shifts of the velocity profile, which occur for drag-reducing surfaces, positive , ΔU+>0\Delta U^{+}>0, and downward shifts of the velocity profile, which occur for drag-increasing surfaces, negative, ΔU+<0\Delta U^{+}<0, so our ΔU+\Delta U^{+} is the opposite of the usual ‘roughness function’ used for drag-increasing textures. The free-stream velocity, Uδ+U_{\delta}^{+}, is then given by

Uδ+=(2cf)1/2=1κlogδ++B+ΔU+,U_{\delta}^{+}=\left(\frac{2}{c_{f}}\right)^{1/2}=\frac{1}{\kappa}\log\delta^{+}+B+\Delta U^{+}, (1)

where cfc_{f} is the skin friction coefficient based on UδU_{\delta}, δ\delta is the flow thickness, and the von Kármán constant, κ\kappa, and the parameter BB, which includes the smooth-wall logarithmic intercept and the wake function, remain unchanged. When considering boundary layers, δ\delta is the boundary-layer thickness. For channels, δ\delta is the channel half-height and we take the centreline velocity as UδU_{\delta}, to allow for direct comparison with boundary layers (García-Mayoral & Jiménez, 2011; García-Mayoral et al., 2019). Following equation 1, the relative change in drag compared to a smooth-wall flow at the same ReτRe_{\tau} is

Δcfcf0=1(1+ΔU+/Uδ0+)21,\frac{\Delta c_{f}}{c_{f0}}=\frac{1}{(1+\Delta U^{+}/U_{\delta 0}^{+})^{2}}-1, (2)

where the subscript ‘0’ denotes reference smooth-wall values and Δcf=cfcf0\Delta c_{f}=c_{f}-c_{f0}.

In the limit where the size of the texture elements, LL, is vanishingly small compared to any length scales in the overlying flow, the background turbulence does not perceive the detail of each individual texture element, and only experiences the surface in an averaged sense. Such surfaces are well suited for homogenisation and can be characterised through uniform effective boundary conditions (Lācis & Bagheri, 2017; Bottaro, 2019). Modelling textured surfaces by homogeneous boundary conditions is convenient and computationally cheap, since high resolution is not required near the surface to resolve the flow around the texture elements. However, homogenisation relies on a small-parameter expansion on the ratio of LL to the characteristic lengthscales in the flow, so it formally ceases to apply when LL becomes comparable to the size of the smallest eddies in the flow, which taking for the latter the diameter of quasi-streamwise vortices would be L+10L^{+}\sim 10. This limit would leave out most practical applications. Here, we aim to investigate the effect on turbulence of textures beyond this vanishingly small limit, i.e. once homogenisation breaks down. As a first step, in this paper, we focus on the particularly simple case of surface textures made of alternating slip/no-slip regions, which is a common model for superhydrophobic surfaces.

In this case, the resulting homogenised boundary conditions are v=0v=0 in the wall-normal direction and u=x(u/y)u=\ell_{x}(\partial u/\partial y) and w=z(w/y)w=\ell_{z}(\partial w/\partial y) in the wall-parallel directions, where x\ell_{x} and z\ell_{z} are the streamwise and spanwise slip lengths (Philip, 1972). Gómez-de-Segura & García-Mayoral (2020) and Ibrahim et al. (2021) showed that the effect of these homogenised boundary conditions is a mere offset of the origins perceived by different flow components, while turbulence remains essentially the same as over smooth walls. A streamwise slip shifts the mean velocity profile by the slip velocity, reducing the drag, while a spanwise slip allows quasi-streamwise vortices, an essential part of the near-wall turbulent cycle, to move closer to the surface (Luchini, 1996; Min & Kim, 2004), increasing the drag. Fairhall & García-Mayoral (2018) showed that for surfaces modelled using slip lengths, ΔU+\Delta U^{+} equals the offset of the virtual origin perceived by mean flow, x+\ell_{x}^{+}, and the one perceived by turbulence, T+\ell_{T}^{+}. Gómez-de-Segura & García-Mayoral (2020) and Ibrahim et al. (2021) showed that T+\ell_{T}^{+} is governed by the interplay between the spanwise slip, z+\ell_{z}^{+}, and the transpiration. For surfaces with no transpiration, such as the cited slip/no-slip patterns, the virtual origin of turbulence only depends on the spanwise slip length, and Fairhall & García-Mayoral (2018) proposed

T+z+1+z+/4.\ell_{T}^{+}\approx\frac{\ell_{z}^{+}}{1+\ell_{z}^{+}/4}. (3)

from an empirical fit of the results of Busse & Sandham (2012).

Seo & Mani (2016) investigated the limits of slip-length models for slip/no-slip textures, and showed that for texture sizes L+10L^{+}\gtrsim 10, the instantaneous correlation between velocity and shear at the surface was lost, which would appear to set the upper limit for the applicability of a slip-length model. Fairhall & García-Mayoral (2018) later investigated the correlation between surface velocity and shear using a spectral approach to discriminate between the slip lengths experienced by different lengthscales in the overlying flow. They found that even scales much larger than the texture size displayed an apparent loss of correlation. Fairhall & García-Mayoral (2018) argued that this observed loss of correlation of the slip length was due to the intensity of the texture-coherent flow, rather than the texture size, becoming significant. We note that Jelly et al. (2014) and Türk et al. (2014) reported that the texture-coherent flow becomes significant compared to the background turbulence for L+100L^{+}\gtrsim 100, while the effect discussed by Fairhall & García-Mayoral (2018) sets in for L+10L^{+}\gtrsim 10, and is caused by the discrete slip/no-slip pattern induced by the texture being broad-band in wavelength space, scattering the texture-coherent signal across the full range of lengthscales. In a follow-up work, Fairhall et al. (2019) used the amplitude-modulated flow decomposition proposed by Abderrahaman-Elena et al. (2019) to filter out the texture-coherent flow, and showed that the left-over background turbulence still exhibits a linear correlation between velocity and shear, so that a slip length can be meaningfully defined.

However, when replacing the texture by the homogeneous slip lengths perceived by the overlying turbulence, results differed for L+25L^{+}\gtrsim 25, as the turbulent variables become no longer smooth-wall-like. Fairhall et al. (2019) suggested that the breakdown of the homogeneous, slip-length model is not caused by the breakdown of the effective boundary conditions, but by a different mechanism. They showed that the difference in ΔU+\Delta U^{+} between the flows over their textures and the flows with equivalent homogeneous boundary conditions arose from modifications to the Reynolds stress above rather than directly at the surface. For the simple case of slip/no-slip textures, this is particularly clear because the zero-transpiration boundary condition (v=0v=0) yields zero Reynolds stress, uvuv, at the surface. For the textures of Fairhall et al. (2019), the differences in uvuv occurred at heights 5y+255\lesssim y^{+}\lesssim 25 above the surface. Fairhall et al. (2019) argued that the extra Reynolds stress over textures was caused by the non-linear interactions between the texture-coherent flow and the background turbulence, which modify the dynamics of the latter and result in degraded drag. We note that although these observations were made in the context of drag-reducing, zero-transpiration textures, we have also observed a similar behaviour for drag-increasing surfaces such as roughness (Abderrahaman-Elena et al., 2019), small-size dense canopies (Sharma & García-Mayoral, 2020b) and porous substrates (Hao & García-Mayoral, 2024), which suggests that this may be a common mechanism across a wide variety of textures. Abderrahaman-Elena et al. (2019) argued that a virtual-origin framework alone could only account for roughness functions up to ΔU+2-\Delta U^{+}\approx 2, spanning the early stages of the transitionally rough regime. The same conclusion was reached in Habibi Khorasani et al. (2022) using homogenised boundary conditions.

In this paper, we aim to identify and characterise the physical mechanism that causes the flow to depart from its dynamics under equivalent boundary conditions in the presence of actual, resolved textures for L+25L^{+}\gtrsim 25. In particular, we assess if the effect of the texture can be captured by replacing it by its corresponding homogeneous boundary conditions plus, critically, the advective terms that arise from the existence of a texture-coherent flow and its interaction with the background turbulence. Compared to Navier-Stokes, the momentum equations for the background turbulence include then additional, ‘forcing’ cross advective terms. We also explore preliminarily if this can be used for predictive modelling using a priori surrogates for the texture-coherent flow.

The paper is organised as follows. The decomposition of the flow field into background-turbulence and texture-coherent components, the resulting governing equations for the mean flow and background turbulence, and the cross non-linear terms that we will introduce in our texture-less model are presented in §2. The numerical methods are outlined in §3. The results from the model with forcing are presented, analysed and compared with those of texture-resolved and homogeneous-slip simulations in §4. Conclusions are summarised in §5.

2 Flow decomposition and governing equations

2.1 Amplitude-modulated triple decomposition

Conventional triple decomposition is often used to obtain a texture-coherent and a texture-incoherent flow component. It decomposes the flow into a space-time-averaged mean flow, a time-averaged component which is phase-locked to the texture, and the remaining time-space fluctuations. Taking for instance the streamwise component of the velocity, we have

u(x,y,z,t)=U(y)+u(x,y,z,t)=U(y)+u~u(x~,y,z~)+uT(x,y,z,t),\begin{split}u(x,y,z,t)&=U(y)+u^{\prime}(x,y,z,t)\\ &=U(y)+\widetilde{u}_{u}(\widetilde{x},y,\widetilde{z})+u_{T}(x,y,z,t),\end{split} (4)

where xx, yy and zz denote the streamwise, wall-normal and spanwise directions respectively, U(y)U(y) is the mean velocity profile, and u(x,y,z,t)u^{\prime}(x,y,z,t) is the full fluctuating field. The latter is further decomposed into a texture-coherent component, or dispersive flow, u~u(x~,y,z~)\widetilde{u}_{u}(\widetilde{x},y,\widetilde{z}), where x~\widetilde{x} and z~\widetilde{z} refer to the local coordinates within the texture period, and the remaining incoherent, background turbulent fluctuations uT(x,y,z,t)u_{T}(x,y,z,t). The texture-coherent component can be viewed as being driven by the existence of a large-scale (mean) streamwise flow, which we denote by the subscript in u~u\widetilde{u}_{u}. The decomposition of equation 4 has been commonly used to separate a texture-coherent contribution from the texture-incoherent, background turbulence (Cheng & Castro, 2002; Nikora et al., 2007; Coceal et al., 2007).

Abderrahaman-Elena et al. (2019), however, showed that this conventional triple decomposition does not produce a uTu_{T} free of coherence with the surface texture. They argued that the texture-coherent flow occurs in response to the background flow, and for any given texture element it would then be driven by the full local signal of the overlying flow, which might be more or less intense than the mean U(y)U(y). The texture-coherent flow would thus be modulated in intensity by the local background turbulence. In the above equation 4, the texture-coherent streamwise velocity, u~u\widetilde{u}_{u}, driven by an overlying streamwise velocity, would be modulated by the streamwise background turbulence, giving

u(x,y,z,t)U(y)+uT(x,y,z,t)+U(y)+uT(x,y,z,t)U(y)u~u(x~,y,z~).u(x,y,z,t)\approx U(y)+u_{T}(x,y,z,t)+\frac{U(y)+u_{T}(x,y,z,t)}{U(y)}\widetilde{u}_{u}(\widetilde{x},y,\widetilde{z}). (5)

In general, however, the overlying flow induces a velocity field around texture elements in all three directions, while itself has also components in all three directions. The spanwise background flow would for instance induce a texture-coherent, spanwise w~w\widetilde{w}_{w}. Therefore, all three texture-coherent velocity components would have contributions induced by all three components of the overlying flow, such that equation 5 would have additional terms for u~w\widetilde{u}_{w} and u~v\widetilde{u}_{v}, the streamwise velocities induced by the background wTw_{T} and vTv_{T}. To illustrate this idea, figure 1 shows a sketch of the streamwise and spanwise overlying velocities inducing coherent flow. Applied to all velocity components, the amplitude-modulated triple decomposition of Abderrahaman-Elena et al. (2019) can be written as the product of a matrix and a vector,

Refer to caption

              overlying streamwise velocity, U+uTU+u_{T}                                                              overlying spanwise velocity, wTw_{T}                           overlying streamwise (cf. spanwise) velocity                      xx (cf. zz)            yy                                          v~u\widetilde{v}_{u} (cf. v~w\widetilde{v}_{w})                                                                    v~u\widetilde{v}_{u} (cf. v~w\widetilde{v}_{w})                  u~u\widetilde{u}_{u}                                          u~u\widetilde{u}_{u}                         w~u\widetilde{w}_{u}                        w~u\widetilde{w}_{u}                                             xx                                                      zz                                                          u~w\widetilde{u}_{w}                                                                              u~w\widetilde{u}_{w}                                                                   w~w\widetilde{w}_{w}                                                                  w~w\widetilde{w}_{w}

Figure 1: Sketch of the texture-coherent flow induced by an overlying velocity in the streamwise or spanwise direction. The blue lines represent streamlines of the induced flow.
𝒖=[u~u/U+1u~v/vu~w/wv~u/Uv~v/v+1v~w/ww~u/Uw~v/vw~w/w+1](U+uTvTwT),\boldsymbol{u}=\begin{bmatrix}\widetilde{u}_{u}/U+1&\widetilde{u}_{v}/v^{*}&\widetilde{u}_{w}/w^{*}\\ \widetilde{v}_{u}/U&\widetilde{v}_{v}/v^{*}+1&\widetilde{v}_{w}/w^{*}\\ \widetilde{w}_{u}/U&\widetilde{w}_{v}/v^{*}&\widetilde{w}_{w}/w^{*}+1\end{bmatrix}\begin{pmatrix}U+u_{T}\\ v_{T}\\ w_{T}\\ \end{pmatrix}, (6)

where ww^{*} and vv^{*} denote the direction-conditional averages of ww and vv over individual roughness elements, thus giving a norm for the intensity of the respective texture-coherent velocities. Abderrahaman-Elena et al. (2019) showed that this modified form of the triple decomposition was more effective at removing the footprint of the texture from 𝒖𝑻\boldsymbol{u_{T}}.

2.2 Governing equations for the background turbulence in flows over textures

Let us now derive the governing equations for the background-turbulence component, and in particular the terms that account for the non-linear interaction with the texture-coherent flow. In a texture-resolving DNS, the incompressible flow within the channel is governed by continuity, 𝒖=0\nabla\cdot\boldsymbol{u}=0, and the Navier-Stokes equations,

t𝒖+𝒖𝒖=p+ν2𝒖,\partial_{t}\boldsymbol{u}+\nabla\cdot\boldsymbol{u}\boldsymbol{u}=-\nabla p+\nu\nabla^{2}\boldsymbol{u}, (7)

where 𝒖\boldsymbol{u} is the velocity vector with components uu, vv, ww. Using the velocity decompositions introduced in section 2.1, the governing momentum equations for the background turbulence can be derived by subtracting the momentum equation for texture-coherent flow from the triple-decomposed Navier-Stokes equations. We apply this first for the case of conventional triple decomposition, as a simpler example that serves us to illustrate the concept, and then apply it for the case of amplitude-modulated decomposition.

2.2.1 Texture-coherent flow obtained from conventional triple decomposition

Using conventional triple decomposition, the velocity vector can be written as

𝒖=(U+u~u+uTv~u+vTw~u+wT),\boldsymbol{u}=\begin{pmatrix}U+\widetilde{u}_{u}+u_{T}\\ \widetilde{v}_{u}+v_{T}\\ \widetilde{w}_{u}+w_{T}\\ \end{pmatrix}, (8)

and the pressure as p=P+p~+pTp=P+\tilde{p}+p_{T}, where PP is the contribution that provides the mean pressure gradient driving the flow. Substituting the triple-decomposed velocities and pressure into the Navier-Stokes equations and taking the temporal and spatial average, we obtain the momentum equation for the mean flow 𝑼=(U,0,0)\boldsymbol{U}=(U,0,0),

𝒖𝑻𝒖𝑻¯+𝒖~𝒖𝒖~𝒖=P+ν2𝑼,\nabla\cdot\left<\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}\right>+\nabla\cdot\left<\boldsymbol{\widetilde{u}_{u}}\boldsymbol{\widetilde{u}_{u}}\right>=-\nabla P+\nu\nabla^{2}\boldsymbol{U}, (9)

where ()\left<\left(\cdot\right)\right> denotes spatial averaging in the wall-parallel directions and ()¯\overline{\left(\cdot\right)} denotes temporal averaging. This has the usual form of the mean-flow equation for rough-wall flows, with the Reynolds and the dispersive stress on left hand side. While the dispersive stress can be significant for other textures, for the present slip/no-slip textures it is negligible compared to the Reynolds stress at least for L+50L^{+}\lesssim 50, only becoming relevant for texture sizes L+70L^{+}\gtrsim 70, as shown in figure 2.

Refer to caption
Figure 2: Reynolds and dispersive stress for slip/no-slip collocated square posts at Reτ180Re_{\tau}\approx 180. Blue to red, L+18L^{+}\approx 18, 24, 35, 47, 71 and 94. , total shear Reynolds stress; , dispersive stress.

The momentum equation for the texture-coherent fluctuation, 𝒖~𝒖\boldsymbol{\widetilde{u}_{u}}, can be obtained by taking the temporal average of the triple-decomposed Navier-Stokes equations and subtracting the momentum equation for 𝑼\boldsymbol{U}, equation 9, which gives

𝑵𝒄=p~+ν2𝒖~𝒖,\boldsymbol{N_{c}}=-\nabla\widetilde{p}+\nu\nabla^{2}\boldsymbol{\widetilde{u}_{u}}, (10)

where

𝑵𝒄=(𝑼+𝒖~𝒖)(𝑼+𝒖~𝒖)𝒖~𝒖𝒖~𝒖+𝒖𝑻𝒖𝑻¯𝒖𝑻𝒖𝑻¯.\boldsymbol{N_{c}}=\nabla\cdot(\boldsymbol{U}+\boldsymbol{\widetilde{u}_{u}})(\boldsymbol{U}+\boldsymbol{\widetilde{u}_{u}})-\nabla\cdot\left<\boldsymbol{\widetilde{u}_{u}}\boldsymbol{\widetilde{u}_{u}}\right>+\nabla\cdot\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}-\nabla\cdot\left<\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}\right>. (11)

Given that the background turbulence is homogeneous in the wall-parallel directions and statistically steady in time, we have 𝒖𝑻𝒖𝑻¯𝒖𝑻𝒖𝑻¯0\nabla\cdot\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}-\nabla\cdot\left<\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}\right>\approx 0 in the non-linear term 𝑵𝒄\boldsymbol{N_{c}}, and the resulting momentum equation for the texture-coherent fluctuation, 𝒖~𝒖\boldsymbol{\widetilde{u}_{u}}, simplifies then to

(𝑼+𝒖~𝒖)(𝑼+𝒖~𝒖)𝒖~𝒖𝒖~𝒖=p~+ν2𝒖~𝒖.\nabla\cdot(\boldsymbol{U}+\boldsymbol{\widetilde{u}_{u}})(\boldsymbol{U}+\boldsymbol{\widetilde{u}_{u}})-\nabla\cdot\left<\boldsymbol{\widetilde{u}_{u}}\boldsymbol{\widetilde{u}_{u}}\right>=-\nabla\widetilde{p}+\nu\nabla^{2}\boldsymbol{\widetilde{u}_{u}}. (12)

Finally, the momentum equation for the background turbulence can be obtained by subtracting the above momentum equation for 𝒖~𝒖\boldsymbol{\widetilde{u}_{u}} from the full triple-decomposed Navier-stokes equation, yielding

t𝒖𝒃+𝒖𝒃𝒖𝒃+𝑵𝒃=pb+ν2𝒖𝒃,\partial_{t}\boldsymbol{u_{b}}+\nabla\cdot\boldsymbol{u_{b}}\boldsymbol{u_{b}}+\boldsymbol{N_{b}}=-\nabla p_{b}+\nu\nabla^{2}\boldsymbol{u_{b}}, (13)

where 𝒖𝒃=𝑼+𝒖𝑻\boldsymbol{u_{b}}=\boldsymbol{U}+\boldsymbol{u_{T}} includes the mean 𝑼\boldsymbol{U} profile and the background turbulent fluctuations, and is thus the flow we are interested in solving for in our texture-less DNSs, and pb{p_{b}} is the corresponding background pressure, pb=P+pT{p_{b}}=P+p_{T}. The additional non-linear terms, 𝑵𝒃\boldsymbol{N_{b}}, are

𝑵𝒃=𝒖~𝒖𝒖𝑻+𝒖𝑻𝒖~𝒖+𝒖~𝒖𝒖~𝒖,\begin{split}\boldsymbol{N_{b}}=\nabla\cdot\boldsymbol{\widetilde{u}_{u}}\boldsymbol{u_{T}}+\nabla\cdot\boldsymbol{u_{T}}\boldsymbol{\widetilde{u}_{u}}+\nabla\cdot\left<\boldsymbol{\widetilde{u}_{u}}\boldsymbol{\widetilde{u}_{u}}\right>,\end{split} (14)

where 𝒖~𝒖𝒖𝑻+𝒖𝑻𝒖~𝒖\nabla\cdot\boldsymbol{\widetilde{u}_{u}}\boldsymbol{u_{T}}+\nabla\cdot\boldsymbol{u_{T}}\boldsymbol{\widetilde{u}_{u}} are the non-linear interactions of the background turbulence and the texture-coherent flow and 𝒖~𝒖𝒖~𝒖\nabla\cdot\left<\boldsymbol{\widetilde{u}_{u}}\boldsymbol{\widetilde{u}_{u}}\right> is the dispersive stress, which acts only on the mean flow 𝑼\boldsymbol{U}. The presence of surface texture thus modifies the background turbulence through these non-linear terms.

2.2.2 Texture-coherent flow obtained from amplitude-modulated triple decomposition

Let us now derive the momentum equations for the background turbulence using the amplitude-modulated triple decomposition of equation 6. For the present case of slip/no-slip textures, we make the following simplifications. At the surface, the wall-normal velocity vv is zero throughout, and therefore any flow induced by the background vv is small, as reported in Fairhall et al. (2019), so we neglect u~v\widetilde{u}_{v}, v~v\widetilde{v}_{v} and w~v\widetilde{w}_{v} in equation 6. Let us however note that this vv-induced flow could be important for protruding textures such as pyramids, cones, and roughness in general. In addition, we also neglect the flow induced by the background ww, since the latter is weak compared to the background streamwise flow for slip/no-slip textures, as also reported in Fairhall et al. (2019). The dominant texture-coherent effect is then the flow induced by streamwise velocity U+uTU+u_{T}, and the modulated triple decomposition simplifies then to

𝒖=(𝑰+[u~u/U00v~u/U00w~u/U00])(U+uTvTwT),=(𝑰+𝑪)𝒖𝒃,\begin{split}\boldsymbol{u}&=\left(\boldsymbol{I}+\begin{bmatrix}\widetilde{u}_{u}/U&0&0\\ \widetilde{v}_{u}/U&0&0\\ \widetilde{w}_{u}/U&0&0\end{bmatrix}\right)\cdot\begin{pmatrix}U+u_{T}\\ v_{T}\\ w_{T}\\ \end{pmatrix},\\ &=\left(\boldsymbol{I}+\boldsymbol{C}\right)\cdot\boldsymbol{u_{b}},\end{split} (15)

where we assume that 𝒖~u\widetilde{\boldsymbol{u}}_{u} can still be obtained by ensemble averaging (Abderrahaman-Elena et al., 2019; Fairhall et al., 2019) and is therefore still governed by equation 10. Similarly, the pressure is decomposed into

p=P+pT+U+uTUp~u,p=P+p_{T}+\frac{U+u_{T}}{U}\widetilde{p}_{u}, (16)

which can be further written as

p=pb+𝑸𝒖𝒃,p=p_{b}+\boldsymbol{Q}\cdot\boldsymbol{u_{b}}, (17)

where 𝑸=[p~u/U00]\boldsymbol{Q}=[\widetilde{p}_{u}/U\quad 0\quad 0], corresponding to a linear expansion about UU.

The Navier-Stokes equations can then be written as

t((𝑰+𝑪)𝒖𝒃)+[((𝑰+𝑪)𝒖𝒃)((𝑰+𝑪)𝒖𝒃)]=(pb+𝑸𝒖𝒃)+ν2((𝑰+𝑪)𝒖𝒃),\begin{split}\partial_{t}\left(\left(\boldsymbol{I}+\boldsymbol{C}\right)\cdot\boldsymbol{u_{b}}\right)+&\nabla\cdot\left[\left(\left(\boldsymbol{I}+\boldsymbol{C}\right)\cdot\boldsymbol{u_{b}}\right)\left(\left(\boldsymbol{I}+\boldsymbol{C}\right)\cdot\boldsymbol{u_{b}}\right)\right]\\ &=-\nabla\left(p_{b}+\boldsymbol{Q}\cdot\boldsymbol{u_{b}}\right)+\nu\nabla^{2}\left(\left(\boldsymbol{I}+\boldsymbol{C}\right)\cdot\boldsymbol{u_{b}}\right),\end{split} (18)

Following the procedure in section 2.2.1, the momentum equation for the background flow can be obtained by subtracting the governing equation for texture-coherent flow, equation 10, from equation 18,

t𝒖𝒃+𝒖𝒃𝒖𝒃+𝑵𝒃=pb+ν2𝒖𝒃+𝑹,\partial_{t}\boldsymbol{u_{b}}+\nabla\cdot\boldsymbol{u_{b}}\boldsymbol{u_{b}}+\boldsymbol{N_{b}^{\prime}}=-\nabla p_{b}+\nu\nabla^{2}\boldsymbol{u_{b}}+\boldsymbol{R}, (19)

where

𝑵𝒃=[(𝑪𝒖𝒃)𝒖𝒃+𝒖𝒃(𝑪𝒖𝒃)]+[(𝑪𝒖𝒃)(𝑪𝒖𝒃)](𝑼+𝒖~𝒖)(𝑼+𝒖~𝒖)+𝒖~𝒖𝒖~𝒖,\begin{split}\boldsymbol{N_{b}^{\prime}}&=\nabla\cdot\left[\left(\boldsymbol{C}\cdot\boldsymbol{u_{b}}\right)\boldsymbol{u_{b}}+\boldsymbol{u_{b}}\left(\boldsymbol{C}\cdot\boldsymbol{u_{b}}\right)\right]+\nabla\cdot\left[\left(\boldsymbol{C}\cdot\boldsymbol{u_{b}}\right)\left(\boldsymbol{C}\cdot\boldsymbol{u_{b}}\right)\right]\\ &-\nabla\cdot(\boldsymbol{U}+\boldsymbol{\widetilde{u}_{u}})(\boldsymbol{U}+\boldsymbol{\widetilde{u}_{u}})+\nabla\cdot\left<\boldsymbol{\widetilde{u}_{u}}\boldsymbol{\widetilde{u}_{u}}\right>,\end{split} (20)

and

𝑹=t(𝑪𝒖𝒃)+(𝑸𝒖𝒃)p~ν2(𝑪𝒖𝒃)+ν2𝒖~𝒖.\begin{split}\boldsymbol{R}=\partial_{t}\left(\boldsymbol{C}\cdot\boldsymbol{u_{b}}\right)+\nabla\left(\boldsymbol{Q}\cdot\boldsymbol{u_{b}}\right)-\nabla\widetilde{p}-\nu\nabla^{2}\left(\boldsymbol{C}\cdot\boldsymbol{u_{b}}\right)+\nu\nabla^{2}\boldsymbol{\widetilde{u}_{u}}.\end{split} (21)

Here, we have drawn a parallel with the result using conventional triple decomposition of equation 13 by grouping the additional advective terms into 𝑵𝒃\boldsymbol{N_{b}^{\prime}}, and any other additional terms arising from the amplitude modulation into a residual 𝑹\boldsymbol{R}. In appendix A we report on the magnitude of the latter, and show that 𝑵𝒃\boldsymbol{N_{b}^{\prime}} is the dominant term. We will thus neglect the residual 𝑹\boldsymbol{R} in our model.

Finally, we can derive the momentum equation for the mean velocity 𝑼\boldsymbol{U} analogously to equation 9 by taking the temporal average of equation 19 particularised for the Fourier xx-zz zero mode, that is, for the xx-zz spatial average. This gives

𝒖𝑻𝒖𝑻¯+𝑵𝒎=P+ν2𝑼,\nabla\cdot\left<\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}\right>+\boldsymbol{N_{m}}=-\nabla P+\nu\nabla^{2}\boldsymbol{U}, (22)

where the forcing term 𝑵𝒎\boldsymbol{N_{m}} is

𝑵𝒎=𝒖~𝒖𝒖~𝒖+𝑪𝒖𝑻𝒖𝑻¯+𝒖𝑻𝒖𝑻¯𝑪T+𝑪𝒖𝑻𝒖𝑻¯𝑪T.\boldsymbol{N_{m}}=\nabla\cdot\left<\boldsymbol{\widetilde{u}_{u}}\boldsymbol{\widetilde{u}_{u}}\right>+\nabla\cdot\left<\boldsymbol{C}\cdot\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}+\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}\cdot\boldsymbol{C}^{T}\right>+\nabla\cdot\left<\boldsymbol{C}\cdot\overline{\boldsymbol{u_{T}}\boldsymbol{u_{T}}}\cdot\boldsymbol{C}^{T}\right>. (23)

Here, 𝒖𝑻(𝑪𝒖𝑻)\boldsymbol{u_{T}}\left(\boldsymbol{C}\cdot\boldsymbol{u_{T}}\right) has been rearranged as 𝒖𝑻𝒖𝑻𝑪T\boldsymbol{u_{T}}\boldsymbol{u_{T}}\cdot\boldsymbol{C}^{T} before averaging in time. Integrating the above mean momentum equation in yy gives the following stress balance

νdUdyuTvT¯Nm,x=uτ2δyδ,\nu\frac{dU}{dy}-\left<\overline{u_{T}v_{T}}\right>-N_{m,x}=u_{\tau}^{2}\frac{\delta^{\prime}-y}{\delta^{\prime}}, (24)

where the role of the dispersive Reynolds stress in equation 9 is now played by an extended term Nm,xN_{m,x},

Nm,x=u~uv~u+u~uv~uU2uTvT¯+u~uUuTvT¯+v~uUuTuT¯.N_{m,x}=\left<\widetilde{u}_{u}\widetilde{v}_{u}+\frac{\widetilde{u}_{u}\widetilde{v}_{u}}{U^{2}}\overline{u_{T}v_{T}}+\frac{\widetilde{u}_{u}}{U}\overline{u_{T}v_{T}}+\frac{\widetilde{v}_{u}}{U}\overline{u_{T}u_{T}}\right>. (25)

Nm,xN_{m,x} includes contributions from the background turbulence, and can thus only be calculated from the results in §4 a posteriori in order to verify that the sum of the three stresses in equation 24 is indeed linear. Results of such measurement are portrayed for reference in figure 3 for the collocated textures of sizes L+50L^{+}\gtrsim 50, as for smaller textures the contribution of Nm,xN_{m,x} is negligible. For the sizes portrayed its intensity increases with L+L^{+}, although it remains small compared to the viscous and background Reynolds stress.

Refer to caption
Figure 3: Comparison of viscous stress ( ), shear Reynolds stress ( ), averaged forcing term ( ) and total stress ( ) for FA47, FA71 and FA94.

3 Numerical Method

To investigate the non-linear interaction between background turbulence and texture-coherent flow, direct numerical simulations (DNS) of turbulent channels were conducted. The numerical code is adapted from that of Fairhall et al. (2019), and is briefly summarised here. The three-dimensional incompressible Navier-Stokes equations are solved using a spectral discretisation in the streamwise and spanwise directions with the wall-normal direction discretised by second-order finite differences on a staggered grid. A fractional step method (Kim & Moin, 1985), combined with a three-step Runge-Kutta scheme, is used to advance in time, with a semi-implicit scheme used for the viscous terms and an explicit scheme for the advective terms (Le & Moin, 1991). The simulations were run with constant mean pressure gradients, adjusted to achieve the desired friction Reynolds numbers, Reτ. The channel is of size 2πδ×πδ×2δ2\pi\delta\times\pi\delta\times 2\delta in the streamwise, spanwise and wall-normal directions respectively, where δ\delta is the channel half-height. Once a statistically steady state was reached, statistics were obtained over 10 times the characteristic largest-eddy-turnover time, δ/uτ\delta/u_{\tau}.

Three sets of DNSs were conducted. The first set consists of texture-resolving simulations with patterns of alternating regions of slip/no-slip boundary conditions on the channel walls. The first set used the DNS code from Fairhall et al. (2019) unmodified. The surfaces are assumed rigidly flat, which leads to zero transpiration. This is a widely used idealisation for superhydrophobic surfaces, where the free-slip regions represent the gas pockets, and the no-slip regions the exposed tips of solid posts. The assumption of free slip is reasonable if the gas pockets are sufficiently deep (Schönecker et al., 2014). The assumption of flat, rigid interfaces is reasonable for L+30L^{+}\lesssim 30 for typical applications (Seo & Mani, 2018). We note nevertheless that in this study we use this model to keep the surface texture as simple as possible, regardless of whether the model is a suitable representation or not of superhydrophobic textures. The latter question is out of the scope of this work.

We consider texture elements consisting of periodic arrays of square posts, both in collocated and staggered arrangements, as illustrated in figure 4, with a solid fraction, the ratio of post area to total surface area, ϕs1/9\phi_{s}\approx 1/9. The texture unit is a square of side LL, repeated periodically in the streamwise and spanwise directions. For our different simulations, the texture size ranges from L+L^{+}\approx 18 to 94 for the collocated textures and L+L^{+}\approx 33 to 66 for the staggered textures.

Refer to caption
Figure 4: Schematic of collocated- and staggered-post arrangements for periodic textures.

The second set of DNSs replaces the textured surfaces by their corresponding homogeneous slip lengths, obtained a posteriori from the corresponding texture-resolving simulations. This set also used the DNS code from Fairhall et al. (2019) unmodified. The last set of DNSs are homogeneous-slip simulations with added forcing terms, with the same slip boundary conditions of the second set. The governing momentum equations have the additional non-linear forcing terms introduced in section 2.2, with the texture-coherent velocities obtained from ensemble-averaging in the texture-resolving simulations.

In order to reduce the computational cost of the texture-resolving simulations, the code uses a multiblock layout, where the near-wall regions have finer grids compared to the channel centre. This is done in order to resolve fully not just the channel turbulence but also the texture-coherent flow, which typically requires higher resolution. In the blocks containing the walls, each texture element is resolved by 24×2424\times 24 grid points in the xx and zz directions. In the central block, the grid resolution is Δx+\Delta x^{+}\approx 8.8 and Δz+\Delta z^{+}\approx 4.4. The latter resolution is also used throughout in the simulations with homogeneous slip. In the wall-normal direction, the grid is stretched, with resolution Δymin+\Delta y_{min}^{+}\approx 0.3 at the surfaces and Δymax+\Delta y_{max}^{+}\approx 3 in the channel centre, and with the fine-xx-zz- resolution blocks extending a height L\approx L into the channel from the wall, which was verified a posteriori to exceed the height at which any fine, texture-induced flow became vanishingly small. Overall, this resulted for instance in roughly 10810^{8} grid points for case TX18 or 2×1072\times 10^{7} for TX47, which can be compared with 2×1062\times 10^{6} for the corresponding smooth-wall and texture-less simulations, or 4×1084\times 10^{8} for TX18 if uniform resolution in xx and zz had been applied throughout.

The texture-resolving and homogeneous-slip simulations with collocated elements with sizes L+18L^{+}\approx 18 to 47 are from Fairhall et al. (2019). Additional simulations with L+71L^{+}\approx 71 and 94, as well as the simulations with staggered elements, have been conducted to complete and expand the database. Simulations with homogeneous slip and added forcing have been conducted matching all the above cases to investigate the effect of the non-linear interaction. The parameters of all three sets of simulations are listed in table 1.

Case      ReτRe_{\tau}      L+L^{+}     Nx,wN_{x,w}     Nz,wN_{z,w}       x+\ell_{x}^{+}       z+\ell_{z}^{+}      ΔU+\Delta U^{+}\!\!\!\!\!
TX18 179.7 17.7 1576 768 5.8 4.0 3.7
TX24 180.2 23.6 1152 576 6.9 4.3 4.1
TX35 179.9 35.3 768 384 8.5 5.0 4.8
TX35H 407.0 35.3 1728 864 8.4 5.1 5.4
TX47 180.1 47.1 576 288 10.0 6.3 5.6
TX71 180.0 70.7 384 192 12.7 7.3 7.5
TX94 179.7 94.2 288 144 14.6 8.5 9.1
TX94H 360.7 94.2 576 288 14.2 10.0 9.7
sTX35 181.0 33.3 576 288 6.0 4.4 3.7
sTX47 180.7 49.9 384 192 7.3 4.7 4.1
sTX71 179.8 66.6 288 144 8.5 3.2 4.7
SL18 179.9 17.7 128 128 5.8 4.0 4.0
SL24 179.9 23.6 128 128 6.9 4.3 5.0
SL35 180.3 35.3 128 128 8.5 5.0 6.5
SL35H 405.4 35.3 256 256 8.4 5.1 6.5
SL47 179.7 47.1 128 128 10.0 6.3 7.8
SL71 179.9 70.7 128 128 12.7 7.3 10.2
SL94 179.9 94.2 128 128 14.6 8.5 12.1
SL94H 359.7 94.2 256 256 14.2 10.0 12.1
sSL35 180.1 33.3 128 128 6.0 4.4 4.2
sSL47 180.4 49.9 128 128 7.3 4.7 5.3
sSL71 180.0 66.6 128 128 8.5 3.2 6.9
FA18 179.9 17.7 128 128 5.8 4.0 3.6
FA24R 180.1 23.6 128 128 6.9 4.3 4.8
FA24 180.0 23.6 128 128 6.9 4.3 4.0
FA24S 180.2 23.6 128 128 6.9 4.3 4.0
FA35R 180.1 35.3 128 128 8.5 5.0 6.0
FA35 179.8 35.3 128 128 8.5 5.0 4.8
FA35S 180.0 35.3 128 128 8.5 5.0 5.0
FA35H 404.7 35.3 256 256 8.4 5.1 5.4
FA47R 180.3 47.1 128 128 10.0 6.3 7.0
FA47 180.2 47.1 128 128 10.0 6.3 5.7
FA71R 180.0 70.7 128 128 12.7 7.3 8.9
FA71 180.1 70.7 128 128 12.7 7.3 7.9
FA94R 179.9 94.2 128 128 14.6 8.5 10.5
FA94 180.0 94.2 128 128 14.6 8.5 9.9
FA94H 359.5 94.2 256 256 14.2 10.0 10.2
sFA35 179.8 33.3 128 128 6.0 4.4 3.6
sFA47 180.3 49.9 128 128 7.3 4.7 4.1
sFA71 180.1 66.6 128 128 8.5 3.2 5.4
Table 1: Simulation parameters for the texture-resolving, slip-only and slip-plus-forcing simulations. For the case names, TX and sTX indicate resolved collocated and staggered textures, SL and sSL slip-only simulations, and FA and sFA simulations with forcing. The number in the case name is approximately the texture size in wall units, L+L^{+}, listed also for texture-less simulations as a reference to the corresponding textured ones. An appended R indicates forcing based on conventional triple decomposition; otherwise the forcing is based on amplitude-modulated decomposition. An appended S indicates the use of an a priori surrogate model for the texture-coherent flow. An appended H indicates higher friction Reynolds number, ReτRe_{\tau}. Nx,wN_{x,w} and Nz,wN_{z,w} are the number of grid points in the streamwise and spanwise directions in the refined blocks that contain the channel walls. x+\ell_{x}^{+} and z+\ell_{z}^{+} are the streamwise and spanwise slip lengths, and ΔU+\Delta U^{+} is the resulting velocity increment away from the wall.

3.1 Dealiasing for the forcing terms

When calculating the product of two variables, such as in the advective term, in discrete Fourier space, the problem of aliasing arises. The convolution of two discrete functions, f^M\hat{f}_{M} and f^N\hat{f}_{N}, containing MM and NN discrete modes, results in a function containing M+NM+N modes. However, if the product function allocated for the convolution, f^P\hat{f}_{P}, is of size P<M+NP<M+N, the excess modes cannot be correctly represented. This additional, high frequency information is then reflected into the resolved modes of the product function.

The method typically used to address this aliasing is to pad f^M\hat{f}_{M} and f^N\hat{f}_{N} with additional modes, with zero value, before the multiplication (Canuto et al., 2012). For the non-linear term (𝒖𝑻𝒖𝑻)\left(\boldsymbol{u_{T}}\boldsymbol{u_{T}}\right) in equation 14, we use the standard ‘2/3 rule’ for dealiasing. All functions have the same size, M=N=PM=N=P, so they need to be padded with an additional N/2N/2 modes to prevent aliasing in f^P\hat{f}_{P} in modes 0 to NN. Aliasing still occurs from the reflection of modes greater than 3N/23N/2 into modes from NN to 3N/23N/2, but this is of no consequence as these modes are discarded once the convolution product has been calculated. In contrast with the standard advection, for the product 𝒖~𝒖𝒖𝑻\boldsymbol{\widetilde{u}_{u}}\boldsymbol{u_{T}}, the convolution of the background turbulence and the texture-coherent flow, the sizes of the two components need not be the same. We have for instance N=128N=128 for 𝒖𝑻\boldsymbol{u_{T}}, with MM different for cases with different texture size, and typically MNM\geq N. Since we are interested in solving only the background turbulence, that is, modes up to NN, for dealiasing in this case we need at least P=N+M/2P=N+M/2, as illustrated in figure 5. Taking case FA35 as an example, in the streamwise direction the texture-coherent component 𝒖~𝒖\boldsymbol{\widetilde{u}_{u}} has M=768M=768 points in discrete Fourier space, so X=128+768/2=512X=128+768/2=512 is required for dealiasing.

Refer to caption
Figure 5: Sketch of the dealiasing strategy for the forcing terms. The spectral region shaded in yellow with modes larger than N+M/2N+M/2 is reflected into the shaded region under the dashed line, which includes only modes larger than NN, and thus avoids aliasing of modes below NN.

4 Results and discussion

In this section, we present and discuss the results of the DNSs summarised in table 1. We first compare the drag predictions obtained from simulations with the texture resolved and those with its effect modelled. Figure 6 portrays those results in terms of the velocity increment ΔU+\Delta U^{+}. For each simulation setup, the figure shows the usual increase of ΔU+\Delta U^{+} with texture size L+L^{+}. The results with resolved textures and with the corresponding slip boundary conditions agree well only up to texture sizes L+20L^{+}\approx 20 (for smaller textures see results in Fairhall et al., 2019) for collocated layouts and L+35L^{+}\approx 35 for staggered ones, although we note that the streamwise spacing between successive rows of posts is then Lx+25L_{x}^{+}\approx 25, close to the collocated value. For larger spacings, using the equivalent homogeneous slip increasingly overpredicts ΔU+\Delta U^{+}, by 35\sim 35% for L+35L^{+}\gtrsim 35 in the case of collocated posts, and by a similar proportion for staggered ones. This difference was already reported by Fairhall et al. (2019). They argued that, given that the effective boundary conditions perceived by the overlying turbulence were the same for texture-resolved and slip simulations, the difference in drag had to arise from differences in the overlying flow. Introducing the forcing terms without amplitude modulation from §2.2.1 improves the prediction of ΔU+\Delta U^{+} for slip-only simulations partially, as shown in Figure 6. The error remains however large, and is only reduced by 30–50%. In turn, introducing the forcing terms with amplitude modulation from §2.2.2 yields values of ΔU+\Delta U^{+} in good agreement with those of texture-resolved simulations at least up to texture sizes L+70L^{+}\approx 70. As the texture size increases further to L+100L^{+}\approx 100, the results begin to depart. Although the deviation remains below 10%, we already expected the forcing model to break down in this range of L+L^{+}, as the assumption gradually ceases to hold that there is sufficient separation of scales between the overlying shear and the texture-coherent flow it induces, rendering the flow decomposition used in the forcing model invalid. This is further discussed in §4.1.

Refer to caption
Figure 6: Comparison of ΔU+\Delta U^{+} obtained from texture-resolved, slip-only and slip-plus-forcing simulations. Full symbols are for Reτ180Re_{\tau}\approx 180, and open symbols for Reτ350Re_{\tau}\approx 350400400. Solid and dashed lines are for simulations with collocated and staggered texture arrangements, respectively. \bullet, texture-resolved simulations; \bullet, simulations with homogeneous slip boundary conditions only; \blacktriangledown, simulations with homogeneous slip plus forcing based on conventional triple decomposition; \blacktriangledown, simulations with homogeneous slip plus forcing based on amplitude-modulated triple decomposition.

For the staggered-posts layouts, the values of ΔU+\Delta U^{+} are lower than for collocated layouts with the same L+L^{+}. This is in agreement with the Stokes-flow predictions for small textures of Sbragaglia & Prosperetti (2007). They argued that collocated textures channel the flow through streamwise-aligned channels between posts, while staggered arrangements obstruct this channelling effect, reducing the mean slip velocity. This obstruction was also important in the simulations of Seo & Mani (2018), who observed that the slip lengths measured from DNSs of surfaces with randomly distributed texture elements was reduced by approximately 30% compared to collocated elements. In any event, the results for texture-resolved, slip-only and slip-plus-forcing simulations for staggered posts follow generally the same trends observed for collocated posts, albeit with lower values of ΔU+\Delta U^{+} for the same L+L^{+}, and are therefore not presented in the remainder of this section. They are nevertheless included for completeness in appendix B.

Refer to caption
Figure 7: R.m.s velocity fluctuations for collocated textures of sizes L+20L^{+}\approx 20100100 at Reτ180Re_{\tau}\approx 180. , texture-resolved simulations; slip-only simulations; , simulations with forcing based on conventional triple decomposition; , simulations with forcing based on amplitude-modulated decomposition.
Refer to caption
Figure 8: Shear Reynolds stress and mean velocity profile for collocated textures of sizes L+20L^{+}\approx 20100100 at Reτ180Re_{\tau}\approx 180. Line styles are as in figure 7.

The agreement exhibited by the roughness function between texture-resolved simulations and texture-less simulations with amplitude-modulated forcing extends to other flow properties. This is the case for instance of one-point turbulent statistics. Figures 7 and 8 portray the r.m.s. velocity fluctuations and the shear Reynolds stress and mean velocity profile for texture-resolved, slip-only and slip-plus-forcing simulations, both using amplitude-modulated and conventional triple decomposition, across the range L+20L^{+}\approx 20100100. For L+20L^{+}\approx 20, even slip-only simulations show good agreement with fully resolved ones. This was reported by Fairhall et al. (2019) as the limit size for which slip-lengths alone could capture the effect of the texture, as the texture-coherent flow is small in amplitude and confined to the immediate vicinity of the surface, and does therefore not alter the background turbulence significantly. The latter remains then smooth-wall like, other than by a shift in apparent origins (Ibrahim et al., 2021). In agreement with this, adding forcing to model the effect of the texture-coherent fluctuations in this L+L^{+} range has little effect and essentially does not alter the flow. As the texture size increases from L+20L^{+}\approx 20, though, the flow begins to depart from the smooth-wall-like behaviour that slip boundary conditions yield, as shown in figures 7 and 8, with a decrease of the streamwise fluctuation intensity above y+10y^{+}\approx 10, and an increase throughout of the spanwise and wall-normal intensities and of the shear Reynolds stress. We note that the latter is in all cases zero at the surface, a unique feature of slip-no slip textures caused by the zero transpiration at y=0y=0. In general, the above modifications, which tend to decay sufficiently away from the wall, roughly at y+y^{+}\approx 50, are observed over slip/no-slip textures (Seo et al., 2015; Fairhall et al., 2019) but also over rough surfaces (Orlandi & Leonardi, 2006; Abderrahaman-Elena et al., 2019).

The addition of forcing using conventional triple decomposition can reproduce some of the departures from smooth-wall-like flow mentioned above for textured simulations, but forcing with amplitude modulation shows much better agreement with the resolved-texture cases. The agreement is excellent up to L+50L^{+}\approx 50 and first begins to break down for the spanwise velocity. This was to be expected given the simplifications made in equation 15, and has little effect on the Reynolds stress and, therefore, on the mean velocity profile and the drag. The agreement breaks down further for L+70L^{+}\approx 70, for which it begins to propagate into ΔU+\Delta U^{+}, although it is still reasonable. For L+100L^{+}\approx 100 the departures become significant. We therefore identify this as the limit beyond which the model proposed here fails.

As mentioned in section 1, the differences in the Reynolds stress profile shown in figure 8 are caused by the changes in the background turbulence. The latter are what the forcing models ultimately aim to capture. The increased Reynolds stress causes a downward shift of the mean velocity profile away from the wall, and a corresponding reduction in ΔU+\Delta U^{+}. This relationship can be quantified by integrating the streamwise momentum equation. Here we follow Gómez-de-Segura & García-Mayoral (2019). A first integral gives

dU+dy++τuv+=δ+y+δ+,\frac{\mathrm{d}U^{+}}{\mathrm{d}y^{+}}+\tau_{uv}^{+}=\frac{\delta^{\prime+}-y^{+}}{\delta^{\prime+}}, (26)

where τuv\tau_{uv} is the shear Reynolds stress, including any dispersive stress, and δ=δ+T\delta^{\prime}=\delta+\ell_{T} is the effective half-height of the channel, which accounts for the background turbulence perceiving a virtual origin at y=Ty=-\ell_{T}. Integrating equation 26 once more in the wall-normal direction, from the surface to a height HH sufficiently far above for all surface effects to have vanished, gives

U+(H+)Uslip++0H+τuv+(y+)dy+=f,U^{+}\left(H^{+}\right)-U^{+}_{\mathrm{slip}}+\int_{0}^{H^{+}}\tau_{uv}^{+}\left(y^{+}\right)\mathrm{d}y^{+}=f, (27)

where Uslip=U(y+=0)U_{\mathrm{slip}}=U(y^{+}=0) is the slip velocity, and ff is a simple function of H+H^{+}, δ+\delta^{\prime+} and T+\ell_{T}^{+}. The same integral can be repeated for a reference smooth-wall flow at the same friction Reynolds number δ+\delta^{\prime+} between the corresponding heights, y=Ty=\ell_{T} and y=H+Ty=H+\ell_{T}, yielding

US+(H++T+)US+(T+)+T+H++T+τuv,S+(yS+)dyS+=f,U_{\mathrm{S}}^{+}\left(H^{+}+\ell_{T}^{+}\right)-U_{\mathrm{S}}^{+}\left(\ell_{T}^{+}\right)+\int_{\ell_{T}^{+}}^{H^{+}+\ell_{T}^{+}}\tau_{uv,\mathrm{S}}^{+}\left(y_{S}^{+}\right)\mathrm{d}y_{S}^{+}=f, (28)

where the subscript S denotes smooth-wall flow. The roughness function ΔU+\Delta U^{+} can then be obtained by subtracting equations 27 and 28,

ΔU+=U+(H+)US+(H++T+)=Uslip+US+(T+)+0H+[τuv+(y+)τuv,S+(y++T+)]dy+.\begin{split}\Delta U^{+}&=U^{+}\left(H^{+}\right)-U_{S}^{+}\left(H^{+}+\ell_{T}^{+}\right)\\ &=U^{+}_{\mathrm{slip}}-U_{\mathrm{S}}^{+}\left(\ell_{T}^{+}\right)+\int_{0}^{H^{+}}\!\!\left[\tau_{uv}^{+}\left(y^{+}\right)-\tau_{uv,\mathrm{S}}^{+}\left(y^{+}+\ell_{T}^{+}\right)\right]\mathrm{d}y^{+}.\end{split} (29)

For slip-only simulations, turbulence is smooth-wall like and the integral in equation 29 is essentially zero (Fairhall et al., 2019; Ibrahim et al., 2021). Near the wall, dU+/dy+1\mathrm{d}U^{+}/\mathrm{d}y^{+}\approx 1, so for x+10\ell_{x}^{+}\lesssim 10 we have Uslip+x+U^{+}_{\mathrm{slip}}\approx\ell_{x}^{+}. From equation 3, we have T+4\ell_{T}^{+}\lesssim 4, so also US+(T+)T+U_{\mathrm{S}}^{+}\left(\ell_{T}^{+}\right)\approx\ell_{T}^{+}. The roughness function reduces then to the offset between the apparent origins for the mean flow and for turbulence, ΔU+x+T+\Delta U^{+}\approx\ell_{x}^{+}-\ell_{T}^{+} (Luchini, 1996). For texture-resolved simulations, however, in addition to this origin offset, the increase in Reynolds stress causes further modifications to the mean velocity profile and the roughness function. Fairhall et al. (2019) observed that for the present slip/no-slip textures, with zero transpiration and dispersive stress at y=0y=0, the contribution from the latter to τuv\tau_{uv} is negligible up to at least texture sizes L+50L^{+}\approx 50, as shown in figure 2. Those modifications would then be essentially caused by changes in the background, texture-incoherent turbulence alone. Figure 8 shows that the forcing model with amplitude modulation is able to capture the effect of these changes on the Reynolds stress, and thus on ΔU+\Delta U^{+}, while the one with conventional triple decomposition captures those changes only partially.

Refer to caption
Figure 9: Spectral energy densities of the velocity fluctuations and the shear Reynolds stress at y+15y^{+}\approx 15 for collocated textures of sizes L+20L^{+}\approx 20100100 at Reτ180Re_{\tau}\approx 180. Shaded contours, texture-resolved simulations; slip-only simulations; , simulations with forcing based on conventional triple decomposition; , simulations with forcing based on amplitude-modulated decomposition.

The modifications in the background turbulence can be observed in more detail in the spectral density maps of the different variables, as those portrayed in figure 9. Such maps show the contributions to the statistics shown in figures 7 and 8 at a given height yy from different streamwise and spanwise lengthscales. Figure 9 displays the energy densities at y+15y^{+}\approx 15, a height of intense r.m.s. fluctuations of the background turbulence and also sufficiently above the surface for the texture-coherent flow to be negligible. As observed by Ibrahim et al. (2021), the signature of turbulence in slip-only simulations is essentially the same as over smooth walls. Compared to those cases, for fully resolved textures there is additional energy in shorter streamwise scales, and also in wider spanwise scales particularly for vv. This effect is negligible for L+20L^{+}\lesssim 20, but becomes increasingly marked for greater L+L^{+}. Figure 9 shows that slip-only models fail to capture this gradual change in the dynamics of the background turbulence for L+25L^{+}\gtrsim 25. The forcing model based on conventional triple decomposition is able to generate some additional energy in shorter and wider scales, but not to the full extent observed in texture-resolved simulations. In contrast, the forcing model based on amplitude modulation can generate energy in all the necessary scales, and results in a good overall collapse of the spectra with that for resolved textures up to L+70L^{+}\approx 70. For larger L+L^{+}, deviations appear first in the core regions of the maps for vv and ww and in streamwise long scales of uu and uvuv. These spectra indicate again that the additional forcing terms based on the amplitude-modulated decomposition can capture the effect of the texture on the background turbulence, while forcing based on conventional triple decomposition shows only a limited improvement compared to slip-only simulations.

Refer to caption
Figure 10: Instantaneous realisations of the fluctuating uu (left), vv (centre) and ww (right) velocity components at y+15y^{+}\approx 15 for L+50L^{+}\approx 50. Top row, texture-resolved simulation, TX47; middle row, slip-only simulation, SL47; bottom row, simulation with amplitude-modulated forcing, FA47. From blue to yellow, values are from -4.0 to 4.0 for uu, from -1.2 to 1.2 for vv, and from -2.2 to 2.2 for ww, all in viscous units.

To illustrate the general appearance of the flow, instantaneous realisations of the three velocity components for texture-resolved, slip-only, and amplitude-modulated-forcing simulations are shown in figure 10 at a height y+15y^{+}\approx 15 for texture size L+50L^{+}\approx 50. This size is large enough to exhibit significant differences across models, yet not so large that the forcing model begins to fail. While the slip-only simulation exhibits canonical, smooth-wall-like-turbulence structures, both the texture-resolving and the forcing-model simulations show a similar disruption of the latter, with a reduction in the coherence of the streamwise velocity for scales of order 1000 wall units, as indicated also by the energy spectra. For the wall-normal and spanwise velocities, the lengthscales of the turbulent eddies are also shorter compared to those over homogeneous slip. At this L+50L^{+}\approx 50, the lengthscales and magnitude of the texture-coherent flow near the wall become comparable to those of the background turbulence. The spectra and instantaneous flow fields suggest a modification of the near-wall dynamics through the disruption of streaks and quasi-streamwise vortices by this texture-coherent flow. The similarity of the amplitude-modulated-forcing flow field and the texture-resolved one suggests that the alteration of the background turbulence by the presence of the texture can also be captured by the forcing model.

Finally, to verify that the expected scaling in viscous units for textures whose effect is confined to the vicinity of the wall (García-Mayoral & Jiménez, 2012) also holds for the corresponding models, in addition to the simulations at Reτ180Re_{\tau}\approx 180 we have conducted simulations at Reτ400Re_{\tau}\approx 400 for the collocated textures of size L+35L^{+}\approx 35 and L+100L^{+}\approx 100. The results support this scaling, and are presented and discussed in appendix C.

4.1 The limit of the forcing model

The preceding discussion has shown how the model based on the amplitude-modulated decomposition works well up to L+70L^{+}\approx 70, and how for L+70L^{+}\approx 70 and L+100L^{+}\approx 100 deviations from the fully resolved simulations are increasingly apparent. We have also mentioned that this is to be expected, as the assumption of separation of scales between the two flow components ceases to hold. The decomposition hinges on the idea that one component, the overlying background turbulence, excites the other, the texture-coherent signature, as the response flow in the immediate vicinity of the texture, which does not necessarily cease to hold once the lengthscales of the two become comparable. The algebraic form, however, as laid out in equation 5 or more generally in equation 6, assumes that the exciting overlying flow is on a much larger scale than the excited one, in the spirit of Luchini et al. (1991). As L+L^{+} increases, the breakdown of scale separation occurs first for the cross flow components, as these are mainly produced by the overlying quasi-streamwise vortices, with length and span of order 200×20200\times 20 wall units, while the streamwise component is mainly produced by the streamwise streaks, with length and span of order 1000×1001000\times 100 wall units (Kline et al., 1967; Blackwelder & Eckelmann, 1979; Smith & Metzler, 1983).

Refer to caption
Figure 11: Correlation over multiple instantaneous realisations of the streamwise velocity uu and shear u/y\partial u/\partial y for texture size L+70L^{+}\approx 70, for wavelengths λx+110\lambda_{x}^{+}\approx 110 to 11001100 and λz+110\lambda_{z}^{+}\approx 110 to 550550 from red to blue. Left panels, magnitudes of uu and u/y\partial u/\partial y; centre and right panels, phases between the two in xx and zz. Top, full velocity signal; bottom, background turbulence component. Dashed lines mark slip-lengths obtained from linear regression of the data displayed.
Refer to caption
Figure 12: Correlation over multiple instantaneous realisations of the streamwise velocity ww and shear w/y\partial w/\partial y for texture size L+70L^{+}\approx 70, for wavelengths λx+110\lambda_{x}^{+}\approx 110 to 11001100 and λz+110\lambda_{z}^{+}\approx 110 to 550550 from red to blue. Left panels, magnitudes of ww and w/y\partial w/\partial y; centre and right panels, phases between the two in xx and zz. Top, full velocity signal; bottom, background turbulence component. Dashed lines mark slip-lengths obtained from linear regression of the data displayed.
Refer to caption
Figure 13: Correlation over multiple instantaneous realisations of the streamwise velocity uu and shear u/y\partial u/\partial y for texture size L+95L^{+}\approx 95, for wavelengths λx+110\lambda_{x}^{+}\approx 110 to 11001100 and λz+110\lambda_{z}^{+}\approx 110 to 550550 from red to blue. Left panels, magnitudes of uu and u/y\partial u/\partial y; centre and right panels, phases between the two in xx and zz. Top, full velocity signal; bottom, background turbulence component. Dashed lines mark slip-lengths obtained from linear regression of the data displayed.
Refer to caption
Figure 14: Correlation over multiple instantaneous realisations of the streamwise velocity ww and shear w/y\partial w/\partial y for texture size L+95L^{+}\approx 95, for wavelengths λx+110\lambda_{x}^{+}\approx 110 to 11001100 and λz+110\lambda_{z}^{+}\approx 110 to 550550 from red to blue. Left panels, magnitudes of ww and w/y\partial w/\partial y; centre and right panels, phases between the two in xx and zz. Top, full velocity signal; bottom, background turbulence component. Dashed lines mark slip-lengths obtained from linear regression of the data displayed.

This difference can be observed in the earlier loss of correlation at the wall between velocity and shear in the spanwise direction. Fairhall et al. (2019) showed that the correlation held well for the background turbulence up to L+50L^{+}\approx 50 for both uu and ww. Figures 12 to 14 extend their analysis to the textures of size L+70L^{+}\approx 70 and L+95L^{+}\approx 95. The figures show that the decomposition using equation 6 still results in an excellent recovery of the correlation between uu and u/y\partial u/\partial y for both texture sizes, both in terms of proportion and phase between them, which makes the value of x\ell_{x} estimated from this data meaningful. The same is however not true for the correlation between ww and w/y\partial w/\partial y, which exhibits a considerable scatter both in terms of phase and magnitude. As a result, it is difficult to define a spanwise slip length z\ell_{z} meaningfully. We note nevertheless that this is of minor importance with regards to setting the effective boundary condition for ww. At these large texture sizes, we have z+7\ell_{z}^{+}\gtrsim 7, and thus the effect of the slip length in the boundary condition for ww in equation 3 is significantly saturated, with variations in z\ell_{z} not resulting in significant variations in T\ell_{T}. In any event, the loss of correlation is indicative of the background turbulence component obtained still being contaminated by some amount of texture-induced signal, and thus of the decomposition produced using equation 6 breaking down.

Refer to caption
Figure 15: Spectral energy densities at y=0y=0 for the full streamwise and spanwise velocity components, uu and ww, and for the corresponding background turbulence components as obtained using the amplitude-modulated decomposition of equation 6, uTu_{T} and wTw_{T}, for collocated square posts of sizes L+35L^{+}\approx 35, 47, 71 and 94.

This breakdown is perhaps even clearer in the spectral densities of the tangential velocity components in the immediate vicinity of the texture, both for the background turbulence and the full texture-resolved flow, as portrayed at y=0y=0 in figure 15. Up to texture size L+50L^{+}\approx 50 the main energetic region that can be observed in the spectra of uu and ww is recovered in the spectra of the background-turbulence components. However, for L+70L^{+}\gtrsim 70, the decomposition can successfully filter out the contributions in the vicinity of the texture harmonics, which is fully attributable to the texture-coherent flow and its modulation in amplitude (Abderrahaman-Elena et al., 2019; Fairhall et al., 2019), but the spectral signature of the background turbulence is visibly altered by the decomposition. This is indicative of equation 6 failing to produce the correct signal for the background turbulence in the latter size range. Figure 15 shows that this happens once the lengthscales of the harmonics induced by the texture begin to overlap significantly with the main spectral region of the background turbulence, that is, once scale separation ceases to hold.

The results for texture sizes L+50L^{+}\gtrsim 50 portrayed in figures 6 to 9 indicate that the deviations from the texture-resolved results first occur for ww^{\prime}, and soon extend to the other velocity components. The contribution of long structures of uu^{\prime} and uvuv^{\prime} is particularly overpredicted, ultimately leading to an overprediction of the shear Reynolds stress and an underprediction of the drag. We note however that, even at L+100L^{+}\approx 100, the amplitude-modulated model performs significantly better than the state-of-the-art slip-only models, even if they fail to capture fully the dynamics at play in texture-resolved simulations.

The present break down of the model for L+70L^{+}\gtrsim 70 does not completely rule out its applicability for larger textures, and rather limits its validity in the present form of equations 15 and 19. It is entirely possible that a formulation of the flow decomposition not requiring scale separation could extend its validity to larger sizes. The present formulation also neglects any texture-coherent flow induced by cross-plane fluctuations. Such contributions to the texture-coherent flow would become increasingly important for larger texture sizes, leading to additional cross-advective forcing terms on the background turbulence. Their absence from the present formulation likely also contributes to its breakdown. Dropping the above simplifications would lead to a significantly more complex formulation, however, and is left for future work.

4.2 Using a priori estimates for the texture-coherent flow

The amplitude-modulated forcing model proposed in this paper shows good agreement with texture-resolved simulations at least up to texture sizes L+70L^{+}\approx 70, both in terms of drag prediction and turbulent statistics and structure. This strongly suggests that the model has successfully identified the key physical mechanisms at play, i.e. the non-linear interactions between the texture-coherent flow and the background turbulence, and is able to reproduce them without resolving the texture elements. Our central aim in the present work was to identify and understand this mechanism, but ultimately it would also be interesting to use this understanding to design predictive tools. The results presented thus far do not have a truly predictive character, as they require a posteriori information on the texture-coherent flow obtained by ensemble averaging of texture-resolved simulations. In order to be fully predictive, the model would instead need a priori estimates of the texture-coherent flow. Such estimates are readily available, and their use is discussed below. The results are good, but we note, however, that this does not add to the understanding of the physical mechanism, and its usefulness as a predictive tool is somewhat limited, as it would still require running DNS-resolution simulations, even if without the texture-related resolution requirements. This is nevertheless a useful first step for the development of future models that circumvent the need for DNS altogether.

As mentioned in §1, Abderrahaman-Elena et al. (2019) observed that the ensemble average flow over small textures resembles the flow induced by a steady homogeneous overlying shear at matching L+L^{+}, which can be obtained from laminar steady simulations of a single periodic unit of texture. This is in essence an extension of the Stokes-flow computations used by Luchini et al. (1991), Kamrin et al. (2010) and Luchini (2013) to predict protrusion heights or slip lengths, with the addition of inertial terms. The laminar computations of Abderrahaman-Elena et al. (2019) were extended for the slip/no-slip textures considered in this paper in Adams (2021). In the latter, a synthetic eddy-viscosity obtained from smooth-wall DNS was added to represent the effect of the background turbulence on the shape of the mean velocity profile under a driving pressure gradient. This eddy viscosity was essentially used so that the laminar computations yielded mean profiles more realistic than Couette or Poiseuille ones, although this only had a marginal effect on the texture-coherent flow, in its weaker regions away from the surface. It is analogue to a Van Driest (1956) or Cess (see Reynolds & Tiederman, 1967) conventional model, but was used instead because the latter was found to produce a poor surrogate for the smooth-wall profile at our low Reτ180Re_{\tau}\approx 180. Compared to the texture-resolved DNSs of Fairhall et al. (2019), the resulting flow fields for L+35L^{+}\approx 35 overpredicted the coherent u~u\widetilde{u}_{u} by roughly 20%, and showed good agreement in v~u\widetilde{v}_{u} and w~u\widetilde{w}_{u}, yielding overall a reasonable estimate for the texture-coherent flow.

Refer to caption
Figure 16: Mean velocity profile, r.m.s velocity fluctuations and Reynolds shear stress for simulations with L+24L^{+}\approx 24 (dashed lines) and L+35L^{+}\approx 35 (solid lines) at Reτ180Re_{\tau}\approx 180. , texture-resolved simulations, TX24 and TX35; , slip-only simulations, SL24 and SL35; , simulations with amplitude-modulated forcing, FA24 and FA35; , simulations with amplitude-modulated forcing using an a priori surrogate for the texture-coherent flow, FA24S and FA35S.
Refer to caption
Figure 17: Spectral energy densities of the velocity fluctuations and the Reynolds shear stress at y+15y^{+}\approx 15 for L+35L^{+}\approx 35 at Reτ180Re_{\tau}\approx 180. Filled contours, texture-resolved simulation, TX35; , slip-only simulation, SL35; , simulation with amplitude-modulated forcing, FA35; , simulation with amplitude-modulated forcing using an a priori surrogate for the texture-coherent flow, FA35S.

As a first step to explore the predictive capabilities of the amplitude-modulated forcing model, we study its performance when the texture-coherent flow from DNSs is replaced by the a priori surrogates of Adams (2021) for L+24L^{+}\approx 24 and L+35L^{+}\approx 35. Results are shown in figures 16 and 17. Figure 16 shows excellent agreement in the r.m.s. velocity fluctuations, the Reynolds shear stress and ΔU+\Delta U^{+}, except for an overshoot in uu^{\prime} for the larger texture L+35L^{+}\approx 35 in the immediate vicinity of the wall, y+15y^{+}\lesssim 15. This is likely caused by the excessive intensity in u~u\widetilde{u}_{u} in the surrogate texture-coherent flow, as mentioned above. The overshoot does nevertheless not propagate into the Reynolds stress or any of the other velocity components, and is also confined to a narrow region near the texture, so it essentially does not alter the drag or the near-wall dynamics and dissipation, mainly governed by cross-plane velocities induced by bursts and quasi-streamwise vortices (Ibrahim et al., 2021; Habibi Khorasani et al., 2022; Jiménez, 2022). Similar results can also be observed in the spectral densities, shown for the three velocity components and the Reynolds shear stress at y+15y^{+}\approx 15 in figure 17 for L+35L^{+}\approx 35. The surrogate texture-coherent flow is able to produce an energetic signature in the same short wavelengths exhibited by texture-resolved simulations and those with forcing based on the a posteriori texture-coherent flow, and not present for smooth-wall or slip-only simulations. Although there is room for improvement, especially in the prediction of the near-wall peak in uu^{\prime}, these results suggest that the need to conduct simulations that resolve the texture can be fully circumvented, and that it is possible to resolve the background turbulence, and predict the drag and other flow properties using only a priori data on the texture detail, significantly reducing computational costs.

5 Conclusions

The simulation and prediction of turbulence over textured surfaces requires a spatial resolution that can be more demanding than that needed to resolve the turbulence itself, and can become prohibitive for texture sizes in the range L+5L^{+}\approx 5-100100. This is a relevant range for applications, and includes the working range for drag-reducing textures and the transitionally rough range for drag-increasing ones, beyond which the effect on drag usually asymptotes. In this paper we have investigated the effect of the texture detailed geometry on the background turbulence, with the ultimate aim to sidestep the need to resolve that geometry directly. As a first approach, we have focused on a particularly simple, idealised texture, consisting of a slip/no-slip pattern on an otherwise flat surface, a popular model for superhydrophobic surfaces. Such slip/no-slip textures have some unique properties that simplify their analysis, namely that the effective boundary conditions for the overlying turbulence are well known and characterised, reducing to slip, Robin conditions for the tangential velocities and zero transpiration; and that the wall-normal velocity and Reynolds stress are zero at the reference, interfacial plane, and remain negligible in its vicinity. This allowed Fairhall et al. (2019) to identify that drag degraded due to additional Reynolds stresses occurring above the surface, rather than arising at the surface and propagating into the flow above. They proposed that such Reynolds stresses had to originate from the non-linear interaction of the texture-coherent flow with the background turbulence. This interaction became significant and could not be neglected for L+25L^{+}\gtrsim 25, and would need to be accounted for in any model in addition to the effective slip boundary conditions, which still held up in this range of sizes and at least up to L+50L^{+}\approx 50,

Following up from Fairhall et al. (2019), we have analysed how the decomposition of the flow into a texture-coherent and a background-turbulence components propagates into the governing equations of the two components separately. We have first decomposed the flow using conventional triple decomposition, which produces a much simpler set of governing equations. However, as observed by Abderrahaman-Elena et al. (2019), this decomposition results in a residual texture-coherent signature in the background turbulence. To separate fully the texture-coherent signal and obtain a texture-incoherent background turbulence, Abderrahaman-Elena et al. (2019) proposed a decomposition in which the latter modulates in amplitude the former. Here we have analysed the governing equations for the background turbulence that result from this decomposition. For both the conventional and the amplitude-modulated triple decomposition, we have argued that the background turbulence is governed by Navier-Stokes equations with additional, forcing terms, arising from the cross advective terms between both flow components.

To assess the above hypothesis, we have conducted a series of simulations in which the background turbulence was fully resolved, but the texture was replaced by the corresponding effective boundary conditions plus the forcing terms in the momentum equations mentioned above. For the formulation based on conventional triple decomposition, the results are partially improved compared to using effective boundary conditions alone. For the formulation based on the amplitude-modulated decomposition, the results show excellent agreement up to texture sizes L+50L^{+}\approx 50, and begin to deviate for L+70L^{+}\approx 70. This is the case both for the prediction of drag and ΔU+\Delta U^{+}, and for the statistical properties of turbulence, including r.m.s. velocity fluctuations, Reynolds stresses and mean velocity profiles. In particular, the addition of forcing terms can accurately generate fluctuations at shorter wavelengths than smooth-wall flows, which are present for geometry-resolved simulations but which the effective boundary conditions are unable to generate on their own. Once deviations begin to occur, for texture sizes L+70L^{+}\gtrsim 70, they first manifest in the spanwise velocity component. This is also the component for which the flow decomposition first begins to break down, likely due to the span of background-turbulence eddies becoming comparable to the texture size earlier than their length, which disrupts the implicit assumption of separation of scales embedded in the amplitude-modulated decomposition. Concurrently, the texture-coherent motions excited not only by the overlying streamwise velocity, but by the cross velocity components, cease to be negligible, and therefore our simplifications in the forcing also cease to hold.

The above results strongly suggest that the key effects of surface texture on the overlying turbulence are imposing a set of effective boundary conditions but, critically, also altering the momentum equations through the non-linear interaction with the texture-coherent flow in the advective terms. While this is useful in terms of identifying physical mechanisms, it falls short in terms of predictive power, as quantifying that interaction requires prior knowledge of the texture-coherent flow, but the latter only becomes available from the postprocessing of fully resolved flows. We have therefore also explored the possibility of using a priori surrogates for the texture-coherent flow, based on the laminar steady flow about a single periodic unit of texture. Preliminary results show good agreement, motivating further work.

The present study has only considered a particularly simple type of surface texture. The results are encouraging, but would need to be further tested in more complex and general textures, mainly roughness. Many of the simplifications possible here, e.g. the effective boundary conditions reducing to homogeneous slip and zero transpiration, or accounting only for the texture-coherent flow induced by the overlying streamwise velocity, will likely not apply in the general case, calling for a more complete and complex framework.

\backsection

[Acknowledgements] Computational resources were provided by the University of Cambridge Research Computing Service under EPSRC Tier-2 grant EP/P020259/1, and by the UK ’ARCHER2’ system under PRACE (DECI-17) project pr1u1702 and EPSRC project e776. For the purpose of open access, the authors have applied a Creative Commons Attribution (CC BY) licence to any Author Accepted Manuscript version arising from this submission.

\backsection

[Declaration of interests]The authors report no conflict of interest.

\backsection

[Author ORCIDs]
Chris Fairhall, https://orcid.org/0000-0002-2529-3650;
R. García-Mayoral, https://orcid.org/0000-0001-5572-2607.

Appendix A Magnitude of the forcing term and the residual in the momentum equations

Refer to caption
Figure 18: Time-r.m.s intensity ψx\psi_{x}^{\prime} of the terms in the streamwise component of the momentum equation derived for the background turbulence assuming amplitude-modulated texture-coherent flow, equation 19, for the case of collocated texture with L+35L^{+}\approx 35. , advective term; , viscous term; , pressure-gradient term; , temporal-derivative term; , non-linear forcing term 𝑵𝒃\boldsymbol{N_{b}^{\prime}}; , residual 𝑹\boldsymbol{R}.
Refer to caption
Figure 19: Time-r.m.s intensity ψy\psi_{y}^{\prime} of the terms in the wall-normal component of the momentum equation derived for the background turbulence assuming amplitude-modulated texture-coherent flow, equation 19, for the case of collocated texture with L+35L^{+}\approx 35. , advective term; , viscous term; , pressure-gradient term; , temporal-derivative term; , non-linear forcing term 𝑵𝒃\boldsymbol{N_{b}^{\prime}}; , residual 𝑹\boldsymbol{R}.
Refer to caption
Figure 20: Time-r.m.s intensity ψz\psi_{z}^{\prime} of the terms in the spanwise component of the momentum equation derived for the background turbulence assuming amplitude-modulated texture-coherent flow, equation 19, for the case of collocated texture with L+35L^{+}\approx 35. , advective term; , viscous term; , pressure-gradient term; , temporal-derivative term; , non-linear forcing term 𝑵𝒃\boldsymbol{N_{b}^{\prime}}; , residual 𝑹\boldsymbol{R}.

This appendix portrays evidence of the relative importance of the forcing term 𝑵𝒃\boldsymbol{N_{b}^{\prime}} and the residual 𝑹\boldsymbol{R} in equation 19. The residual is neglected in the governing equations of the simulations presented in §4 with forcing based on the amplitude-modulated decomposition, and it therefore needs to be small for the proposed model to hold. Conversely, if the magnitude of 𝑵𝒃\boldsymbol{N_{b}^{\prime}} was small, we would expect that retaining this term had little effect on the dynamics of the background turbulence.

Figures 18 to 20 portray the time-r.m.s. magnitude of the different terms in equation 19 from the texture-resolved simulation of collocated posts with texture size L+35L^{+}\approx 35 (case TX35). Figures 18, 19 and 20 portray results for the streamwise, wall-normal and spanwise components of the momentum equation respectively, for a representative set of xx-zz wavenumbers and as a function of height yy. The figures show that the dynamics are mostly dominated by the interplay between temporal and advective terms, but in the vicinity of the wall, for y+10y^{+}\lesssim 10, the forcing term, which is neglected in slip-only simulations, can become comparable to, and even larger that, the latter two. This is particularly the case for the streamwise momentum equation, as illustrated by figure 18, and across the whole range of wavelengths. For the spanwise and wall-normal momentum equations, the explicit contribution of 𝑵𝒃\boldsymbol{N_{b}^{\prime}} appears to be less significant. In turn, the residual is also negligible in the spanwise and wall-normal momentum equations. It is typically a fraction of 𝑵𝒃\boldsymbol{N_{b}^{\prime}} of order 1/4-1/3 in the streamwise one, and thus reasonably smaller than the leading-order terms. These results back up neglecting 𝑹\boldsymbol{R} when implementing the amplitude-modulated forcing model in §4.

Appendix B Simulations for staggered-posts textures

Refer to caption
Figure 21: R.m.s. velocity fluctuations, shear Reynolds stress and mean velocity profile for staggered-posts textures with L+35L^{+}\approx 35-7070. , texture-resolved simulations; , slip-only simulations; , simulations with forcing based on amplitude-modulated decomposition.
Refer to caption
Figure 22: Spectral energy densities of the velocity fluctuations and the Reynolds shear stress at y+15y^{+}\approx 15 for staggered texture arrangements. Shaded contours, texture-resolved simulations; , slip-only simulations; , simulations with forcing based on amplitude-modulated decomposition.

Figures 21 and 22 portray results from the simulations for staggered-posts configurations, as sketched in figure 4. The aim of these simulations was to verify if the forcing model using amplitude-modulated decomposition, first tested for a collocated-posts texture, would also be applicable to other surface arrangements. In additions to simulations fully resolving the texture and simulations with forcing, we have also conducted simulations implementing slip boundary conditions alone, to serve as a benchmark for comparison. These simulations complement and expand the data set of Fairhall et al. (2019).

We have conducted simulations for texture sizes L+35L^{+}\approx 35, 5050 and 7070, aiming to span the size range for which slip-only simulations begin to deviate from texture-resolved ones, yet the texture size is not large enough for the decomposition and the forcing model to break down. The simulation parameters and resulting roughness functions are listed in table 1.

The results follow the same trends of the collocated-textures cases. Figure 21 shows that the r.m.s. velocity fluctuations for texture-resolved simulations exhibit differences with the slip-only ones, which display smooth-wall-like turbulence (Fairhall et al., 2019; Ibrahim et al., 2021). These differences are small for L+35L^{+}\approx 35, but become increasingly pronounced for larger texture sizes. Their most salient features are a decrease in near-wall peak uu^{\prime} and an increase in vv^{\prime} and ww^{\prime}. These differences eventually result in a significant increase in the shear Reynolds stress, and a corresponding downward shift of the mean velocity profile away from the wall. The forcing model is able to accurately capture these differences, and produces results very close to those of texture-resolved simulations, with small deviations first appearing in ww^{\prime}, as discussed in §4 for collocated textures.

The spectral densities portrayed in figure 22 are also consistent with the observations in §4 for collocated textures. Compared to smooth-wall turbulence, in texture-resolving simulations have additional energy particularly in shorter scales in the streamwise direction. Slip-only simulations are not able to produce this modification in turbulence, and their spectrum remains essentially smooth wall like as discussed in Fairhall et al. (2019) and Ibrahim et al. (2021). In contrast, the forcing model is able to produce the spectral energy densities of texture-resolved simulations with excellent agreement.

Appendix C Effect of Reynolds number

Refer to caption
Figure 23: R.m.s. velocity fluctuations, shear Reynolds stress and mean velocity profile for simulations at Reτ180Re_{\tau}\approx 180 (solid) and Reτ400Re_{\tau}\approx 400 (dashed). , TX35; , TX35H; , SL35; , SL35H; , FA35; , FA35H.
Refer to caption
Figure 24: Spectral energy densities of the velocity fluctuations and the Reynolds shear stress at y+15y^{+}\approx 15 for L+35L^{+}\approx 35 and L+100L^{+}\approx 100 at different ReτRe_{\tau}. Grey filled contours, texture-resolved simulations at Reτ180Re_{\tau}\approx 180; , at Reτ400Re_{\tau}\approx 400. Blue filled contours, simulations with forcing based on amplitude-modulated decomposition at Reτ180Re_{\tau}\approx 180; , at Reτ400Re_{\tau}\approx 400.

The main set of simulations discussed in this paper were conducted at Reτ180Re_{\tau}\approx 180. To verify that our observations would scale out to other Reynolds numbers, we have conducted a reduced set of simulations at Reτ400Re_{\tau}\approx 400, otherwise matching in inner scaling setups from the main set, with results shown in figures 23 and 24. We have chosen the collocated layouts with L+35L^{+}\approx 35 and L+100L^{+}\approx 100, as one texture size for which the texture-resolved and the forcing simulations show good agreement between them, but differences with the slip-only simulation, and one texture size for which the forcing model shows signs of breaking down.

The results are consistent with our usual observations for other surface topologies (García-Mayoral & Jiménez, 2012; Fairhall et al., 2019; Sharma & García-Mayoral, 2020a, b; Hao & García-Mayoral, 2024). Near the wall, the same effects are produced in inner units for matching simulations, with results eventually collapsing to smooth wall data at equal ReτRe_{\tau} for y+50y^{+}\gtrsim 50. Differences in this region are observable, but entirely attributable to the variations in ReτRe_{\tau}, as they are the same observed for smooth-wall flows (Moser et al., 1999). These are evidenced for instance in the higher peak levels of the r..m.s. velocity fluctuations and the shear Reynolds stress near y+25y^{+}\gtrsim 25, as shown in figure 23. The spectral densities portrayed in 24 confirm these results. The spectral energy content at each wavelength matches when scaled in inner units for corresponding simulations, with larger-scale content only resolved for the higher Reτ400Re_{\tau}\approx 400, as made possible by the larger simulation domain. Overall, the results suggest that the effect of the model, like the effect of the texture, scales in inner units as expected, and can be extrapolated to and used at different Reynolds numbers.

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