A review of turbulent skin-friction drag reduction by near-wall transverse forcing

P Ricco, M Skote, MA Leschziner - Progress in Aerospace Sciences, 2021 - Elsevier
The quest for reductions in fuel consumption and CO 2 emissions in transport has been a
powerful driving force for scientific research into methods that might underpin drag-reducing …

Equilibrium and non-equilibrium turbulent boundary layers

WJ Devenport, KT Lowe - Progress in Aerospace Sciences, 2022 - Elsevier
This article presents a review of historical and recent developments in the understanding of
equilibrium and non-equilibrium turbulent boundary layers at incompressible high-Reynolds …

Physics-informed neural networks for solving Reynolds-averaged Navier–Stokes equations

H Eivazi, M Tahani, P Schlatter, R Vinuesa - Physics of Fluids, 2022 - pubs.aip.org
Physics-informed neural networks (PINNs) are successful machine-learning methods for the
solution and identification of partial differential equations. We employ PINNs for solving the …

Direct numerical simulation of hypersonic turbulent boundary layers: effect of spatial evolution and Reynolds number

J Huang, L Duan, MM Choudhari - Journal of Fluid Mechanics, 2022 - cambridge.org
Direct numerical simulations (DNS) are performed to investigate the spatial evolution of flat-
plate zero-pressure-gradient turbulent boundary layers over long streamwise domains () …

Turbulent boundary layers around wing sections up to Rec= 1,000,000

R Vinuesa, PS Negi, M Atzori, A Hanifi… - International Journal of …, 2018 - Elsevier
Reynolds-number effects in the adverse-pressure-gradient (APG) turbulent boundary layer
(TBL) developing on the suction side of a NACA4412 wing section are assessed in the …

History effects and near equilibrium in adverse-pressure-gradient turbulent boundary layers

A Bobke, R Vinuesa, R Örlü, P Schlatter - Journal of Fluid Mechanics, 2017 - cambridge.org
Turbulent boundary layers under adverse pressure gradients are studied using well-
resolved large-eddy simulations (LES) with the goal of assessing the influence of the …

Lift-up, Kelvin–Helmholtz and Orr mechanisms in turbulent jets

E Pickering, G Rigas, PAS Nogueira… - Journal of Fluid …, 2020 - cambridge.org
Three amplification mechanisms present in turbulent jets, namely lift-up, Kelvin–Helmholtz
and Orr, are characterized via global resolvent analysis and spectral proper orthogonal …

A theoretical decomposition of mean skin friction generation into physical phenomena across the boundary layer

N Renard, S Deck - Journal of Fluid Mechanics, 2016 - cambridge.org
A theoretical decomposition of mean skin friction generation into physical phenomena
across the whole profile of the incompressible zero-pressure-gradient smooth-flat-plate …

General method for determining the boundary layer thickness in nonequilibrium flows

KP Griffin, L Fu, P Moin - Physical Review Fluids, 2021 - APS
While the computation of the boundary-layer thickness is straightforward for canonical
equilibrium flows, there are no established definitions for general nonequilibrium flows. In …

Spectral proper orthogonal decomposition and resolvent analysis of near-wall coherent structures in turbulent pipe flows

LI Abreu, AVG Cavalieri, P Schlatter… - Journal of Fluid …, 2020 - cambridge.org
Direct numerical simulations, performed with a high-order spectral-element method, are
used to study coherent structures in turbulent pipe flow at friction Reynolds numbers. The …