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20242026
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physics.flu-dyn2026

Can Explicit Subgrid Models Enhance Implicit LES Simulations? A Very High-Order Solver Perspective

Gonzalo Rubio, Gerasimos Ntoukas, Miguel Chávez-Módena +5

The paper studies how explicit Vreman subgrid‑scale models interact with the inherent numerical dissipation of very high‑order discontinuous Galerkin methods for turbulent flow sim…

physics.flu-dyn2026

High-lift Wing Separation Control via Bayesian Optimization and Deep Reinforcement Learning

Ricard MontalÃ, Bernat Font, Oriol Lehmkuhl +2

This study investigates active flow control (AFC) of a 30P30N high-lift wing at a Reynolds number Re = 450,000 and angle of attack = 23 using wallresolved large-ed…

physics.flu-dyn2025

SmartFlow: A CFD-solver-agnostic deep reinforcement learning framework for computational fluid dynamics on HPC platforms

Maochao Xiao, Yuning Wang, Felix Rodach +15

Deep reinforcement learning (DRL) is emerging as a powerful tool for fluid-dynamics research, encompassing active flow control, autonomous navigation, turbulence modeling and disco…

physics.flu-dyn2025

WaterLily.jl: A differentiable and backend-agnostic Julia solver for incompressible viscous flow around dynamic bodies

Gabriel D. Weymouth, Bernat Font

Integrating computational fluid dynamics (CFD) solvers into optimization and machine-learning frameworks is hampered by the rigidity of classic computational languages and the slow…

physics.flu-dyn2025

Flow control of three-dimensional cylinders transitioning to turbulence via multi-agent reinforcement learning

P. Suárez, F. Alcántara-Ávila, J. Rabault +4

Designing active-flow-control (AFC) strategies for three-dimensional (3D) bluff bodies is a challenging task with critical industrial implications. In this study we explore the pot…

physics.flu-dyn2025

Deep-reinforcement-learning-based separation control in a two-dimensional airfoil

Xavier Garcia, Arnau Miró, Pol Suárez +5

The aim of this study is to discover new active-flow-control (AFC) techniques for separation mitigation in a two-dimensional NACA 0012 airfoil at a Reynolds number of 3000. To find…