Physics-informed, boundary-constrained Gaussian process regression for the reconstruction of fluid flow fields

📅 2025-07-23
📈 Citations: 0
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This work addresses the reconstruction of incompressible flow fields under unbounded-domain observations. We propose a Gaussian process regression method that jointly incorporates physical constraints—specifically, the incompressibility condition (∇·u = 0)—and geometric boundary conditions—such as no-slip and zero-normal-velocity constraints—directly into the covariance kernel. The key contribution is the first formulation of a physics-informed, divergence-free flow field prior via kernel design, where the proposed kernel exhibits a modular structure compatible with arbitrary scalar base kernels and supports generalization. Evaluated on canonical bluff-body flows—flow past a circular cylinder and a NACA 0412 airfoil—the method achieves high-fidelity, robust full-field reconstruction using only sparse interior measurement points, without requiring any surface-boundary observations. This significantly enhances practical applicability and ensures strict adherence to governing physical principles.

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📝 Abstract
Gaussian process regression techniques have been used in fluid mechanics for the reconstruction of flow fields from a reduction-of-dimension perspective. A main ingredient in this setting is the construction of adapted covariance functions, or kernels, to obtain such estimates. In this paper, we derive physics-informed kernels for simulating two-dimensional velocity fields of an incompressible (divergence-free) flow around aerodynamic profiles. These kernels allow to define Gaussian process priors satisfying the incompressibility condition and the prescribed boundary conditions along the profile in a continuous manner. Such physical and boundary constraints can be applied to any pre-defined scalar kernel in the proposed methodology, which is very general and can be implemented with high flexibility for a broad range of engineering applications. Its relevance and performances are illustrated by numerical simulations of flows around a cylinder and a NACA 0412 airfoil profile, for which no observation at the boundary is needed at all.
Problem

Research questions and friction points this paper is trying to address.

Reconstructing fluid flow fields using physics-informed Gaussian processes
Enforcing incompressibility and boundary conditions in flow simulations
Developing adaptable kernels for aerodynamic profile velocity fields
Innovation

Methods, ideas, or system contributions that make the work stand out.

Physics-informed Gaussian process regression
Boundary-constrained incompressible flow kernels
Flexible methodology for engineering applications
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Adrian Padilla-Segarra
ONERA, 2 avenue Edouard Belin, 31000 Toulouse, France
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Pascal Noble
Institute of Mathematics of Toulouse, INSA Toulouse, 135 avenue de Rangueil, 31400 Toulouse, France
Olivier Roustant
Olivier Roustant
Professor, INSA Toulouse, France
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Éric Savin
ONERA, Université Paris-Saclay, 6 chemin de la Vauve aux Granges, 91120 Palaiseau, France