[Paper Review] Turbulent skin-friction reduction by wavy surfaces
This study investigates passive skin-friction drag reduction in turbulent channel flows using skewed wavy walls to emulate the shear-strain effects of a Spatial Stokes Layer (SSL) without active actuation. Direct numerical simulations show a net drag reduction of up to 0.5% due to a 2% friction drag reduction, offset by a 1.3% pressure drag penalty, with the transverse shear strain remaining approximately Reynolds-number independent when scaled in wall units.
Direct numerical simulations of fully-developed turbulent channel flows with wavy walls are undertaken. The wavy walls, skewed with respect to the mean flow direction, are introduced as a means of emulating a Spatial Stokes Layer (SSL) induced by in-plane wall motion. The transverse shear strain above the wavy wall is shown to be similar to that of a SSL, thereby affecting the turbulent flow, and leading to a reduction in the turbulent skin-friction drag. The pressure- and friction-drag levels are carefully quantified for various flow configurations, exhibiting a combined maximum overall-drag reduction of about 0.5%. The friction-drag reduction is shown to behave approximately quadratically for small wave slopes and then linearly for higher slopes, whilst the pressure-drag penalty increases quadratically. Unlike in the SSL case, there is a region of increased turbulence production over a portion of the wall, above the leeward side of the wave, thus giving rise to a local increase in dissipation. The transverse shear-strain layer is shown to be approximately Reynolds-number independent when the wave geometry is scaled in wall units.
Motivation & Objective
- To explore passive, geometrically induced drag reduction in turbulent boundary layers using wavy walls as a substitute for active in-plane wall motions.
- To assess whether wavy walls can emulate the transverse shear-strain profile of a Spatial Stokes Layer (SSL), known to reduce skin friction.
- To quantify the trade-off between friction-drag reduction and pressure-drag penalty in wavy-wall configurations.
- To evaluate the Reynolds-number dependence of the shear-strain profile and drag reduction performance when wall geometry is scaled in wall units.
- To identify dominant mechanisms limiting performance, including localized turbulence production and phase variation effects.
Proposed method
- Direct numerical simulations (DNS) of fully developed turbulent channel flows with wavy walls are performed using a spectral/hp element method with high spatial and temporal resolution.
- The wavy wall is oriented at an angle θ to the mean flow direction, generating a spanwise pressure gradient that induces spanwise flow and transverse shear strain.
- The wall geometry is scaled in wall units (e.g., A⁺, λ⁺) to assess Reynolds-number independence of the shear-strain profile.
- Drag components—friction and pressure—are computed and compared against a baseline plane channel flow with identical mesh and domain size.
- Grid convergence studies are conducted at Reτ = 360 to assess numerical accuracy and sensitivity of drag reduction estimates.
- Turbulence production and dissipation terms are analyzed to identify localized instabilities and energy transfer mechanisms near the leeward side of the wave.
Experimental results
Research questions
- RQ1Can a passive wavy wall geometry effectively emulate the transverse shear-strain profile of a Spatial Stokes Layer (SSL) in turbulent channel flow?
- RQ2How does the net drag reduction vary with wave height, wavelength, and flow angle, and what is the optimal configuration?
- RQ3To what extent is the shear-strain profile and drag reduction performance independent of Reynolds number when wall geometry is scaled in wall units?
- RQ4What are the dominant mechanisms limiting drag reduction, particularly in terms of turbulence production and pressure drag?
- RQ5How do localized increases in turbulence production above the leeward side of the wave affect overall energy dissipation and performance?
Key findings
- The transverse shear-strain profile above the wavy wall closely resembles that of a Spatial Stokes Layer (SSL), validating the emulation strategy.
- Friction-drag reduction scales approximately quadratically for small wave slopes and linearly for higher slopes, while pressure-drag penalty increases quadratically with wave height.
- A net drag reduction of approximately 0.5% is estimated at Reτ ≈ 360 for a configuration with A⁺ ≈ 20, λ⁺ ≈ 920, and θ = 70°, based on the finest grid resolution.
- The shear-strain profile is approximately Reynolds-number independent when wall geometry is scaled in wall units, indicating robustness across Reynolds numbers.
- A localized peak in turbulence production is observed above the leeward side of the wave, contributing to increased dissipation and counteracting drag reduction.
- The performance of the wavy wall is limited by a combination of quadratic pressure drag and localized turbulence intensification, which degrades the benefit from friction reduction.
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This review was created by AI and reviewed by human editors.