A review of turbulent skin-friction drag reduction by near-wall transverse forcing
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 …
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 …
equilibrium and non-equilibrium turbulent boundary layers at incompressible high-Reynolds …
Physics-informed neural networks for solving Reynolds-averaged Navier–Stokes equations
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 …
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
Direct numerical simulations (DNS) are performed to investigate the spatial evolution of flat-
plate zero-pressure-gradient turbulent boundary layers over long streamwise domains () …
plate zero-pressure-gradient turbulent boundary layers over long streamwise domains () …
Turbulent boundary layers around wing sections up to Rec= 1,000,000
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 …
(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
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 …
resolved large-eddy simulations (LES) with the goal of assessing the influence of the …
Lift-up, Kelvin–Helmholtz and Orr mechanisms in turbulent jets
Three amplification mechanisms present in turbulent jets, namely lift-up, Kelvin–Helmholtz
and Orr, are characterized via global resolvent analysis and spectral proper orthogonal …
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
A theoretical decomposition of mean skin friction generation into physical phenomena
across the whole profile of the incompressible zero-pressure-gradient smooth-flat-plate …
across the whole profile of the incompressible zero-pressure-gradient smooth-flat-plate …
General method for determining the boundary layer thickness in nonequilibrium flows
While the computation of the boundary-layer thickness is straightforward for canonical
equilibrium flows, there are no established definitions for general nonequilibrium flows. In …
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
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 …
used to study coherent structures in turbulent pipe flow at friction Reynolds numbers. The …