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20102024
most citedPhysics-informed neural networks for solving Reynolds-averaged Navier$\unicode{x2013}$Stokes equations

481 citations · 1.2k across the 57 of their papers we have counts for

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Showing 2018Show all

7 papers · 1 filter

physics.flu-dyn2018★ 8 cited

Assessment of skin-friction-reduction techniques on a turbulent wing section

M. Atzori, R. Vinuesa, A. Stroh +2

The scope of the present project is to quantify the effects of uniform blowing and body-force damping on turbulent boundary layers subjected to a non-uniform adverse-pressure-gradi…

physics.flu-dyn2018

History effects for cambered and symmetric wing profiles

A. Tanarro, R. Vinuesa, P. Schlatter

The characteristics of complex turbulent boundary layers under adverse pressure gradients are assessed through well-resolved large-eddy simulations (LES) with the spectral-element…

physics.flu-dyn2018

Revisiting the amplitude modulation in wall-bounded turbulence: towards a robust definition

E. Dogan, R. Örlü, D. Gatti +2

The present study revisits the amplitude modulation phenomenon, specifically for the robustness in its quantification. To achieve this, a well-resolved large-eddy simulation (LES)…

physics.flu-dyn2018★ 1 cited

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

P. Schlatter, R. Vinuesa, A. Bobke +1

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 streamwise p…

physics.flu-dyn2018

Assessment of turbulent boundary layers on a NACA4412 wing section at moderate Re

R. Vinuesa, S. M. Hosseini, A. Hanifi +2

The results of a DNS of the flow around a wing section represented by a NACA4412 profile, with Rec = 400, 000 and 5 degree angle of attack, are presented in this study. The high-or…

physics.flu-dyn2018

Reynolds-number effects in turbulent boundary layers around wing sections

Ricardo Vinuesa, Prabal Negi, Marco Atzori +3

Four well-resolved LESs of the turbulent boundary layers around a NACA4412 wing section, with Rec ranging from 100,000 to 1,000,000, were performed at 5 degree angle of attack. By…