Physics-informed, boundary-constrained Gaussian process regression for the reconstruction of fluid flow fields
- URL: http://arxiv.org/abs/2507.17582v2
- Date: Wed, 17 Sep 2025 15:25:52 GMT
- Title: Physics-informed, boundary-constrained Gaussian process regression for the reconstruction of fluid flow fields
- Authors: Adrian Padilla-Segarra, Pascal Noble, Olivier Roustant, Éric Savin,
- Abstract summary: We present a general method for constraining a prescribed Gaussian process on an arbitrary compact set.<n>We derive physics-informed kernels for simulating two-dimensional velocity fields of an incompressible (divergence-free) flow around aerodynamic profiles.<n>The relevance of the methodology and performances are illustrated by numerical simulations of flows around a cylinder and a NACA 0412 airfoil profile.
- Score: 0.6999740786886536
- License: http://arxiv.org/licenses/nonexclusive-distrib/1.0/
- 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 present a general method for constraining a prescribed Gaussian process on an arbitrary compact set. The kernel of the pre-defined process must be at least continuous and may include other information about the studied phenomenon. This general boundary-constraining framework can be implemented with high flexibility for a broad range of engineering applications. From this, 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. We describe an adapted numerical method for the boundary-constraining procedure parameterized by a measure on the compact set. The relevance of the methodology 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.
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