As the Reynolds number increases, the large-eddy simulation (LES) of complex flows becomes increasingly intractable because near-wall turbulent structures become increasingly small. Wall modeling reduces the computa-tional requirements of LES by enabling the use of coarser cells at the walls. This paper presents a machine-learning methodology to develop data-driven wall-shear-stress models that can directly operate, a posteriori, on the unstruc-tured grid of the simulation. The model architecture is based on graph neural networks. The model is trained on a database which includes fully developed boundary layers, adverse pressure gradients, separated boundary layers, and laminar-turbulent transition. The relevance of the trained model is verified a posteriori for the simulation of a channel flow, a backward-facing step and a linear blade cascade.
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Univ Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, ItalyUniv Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, Italy
Gualtieri, P.
Casciola, C. M.
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Univ Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, ItalyUniv Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, Italy
Casciola, C. M.
Benzi, R.
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Univ Roma Tor Vergata, Dipartimento Fis, I-00133 Rome, Italy
Univ Roma Tor Vergata, INFM, I-00133 Rome, ItalyUniv Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, Italy
Benzi, R.
Piva, R.
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Univ Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, ItalyUniv Roma La Sapienza, Dipartimento Meccan & Aeronaut, I-00184 Rome, Italy