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📄 Abstract
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.