20th AIAA Computational Fluid Dynamics Conference 2011
DOI: 10.2514/6.2011-3047
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Euler/Navier-Stokes couplings for multiscale aeroacoustic problems

Abstract: We present in this paper two Euler/Navier-Stokes couplings for multiscale aeroacoustic problems based on a Discontinuous Galerkin method: the first coupling concerns an interface coupling between adjacent domains, the second coupling concerns a coupling in volume and interface between overlapping domains. In both cases, each domain provide a donor field to the other domain. After a numerical study of the convergence of the precision of the method, these couplings are compared on a 2D test case of a flow around… Show more

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Cited by 4 publications
(4 citation statements)
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“…In these works, different numerical schemes are applied in the atomistic and continuum regions, each restricted to its own subdomain, and the transfer of information from the continuum to the atomistic scale occurs in the overlap region. Schwarz-like methods have also been proposed to couple distinct physics in different subdomains, for example, fluid-structure interaction (Engel and Griebel [18]), and computational fluid dynamics with aero-acoustics (Borrel, Halpern, and Ryan [13] and Ryan, Halpern, and Borrel [52]). In these works, the governing equations are solved alternatively in each subdomain, and the necessary information, such as structure-fluid loading, is transferred through boundary conditions at the interface.…”
Section: Previous Workmentioning
confidence: 99%
“…In these works, different numerical schemes are applied in the atomistic and continuum regions, each restricted to its own subdomain, and the transfer of information from the continuum to the atomistic scale occurs in the overlap region. Schwarz-like methods have also been proposed to couple distinct physics in different subdomains, for example, fluid-structure interaction (Engel and Griebel [18]), and computational fluid dynamics with aero-acoustics (Borrel, Halpern, and Ryan [13] and Ryan, Halpern, and Borrel [52]). In these works, the governing equations are solved alternatively in each subdomain, and the necessary information, such as structure-fluid loading, is transferred through boundary conditions at the interface.…”
Section: Previous Workmentioning
confidence: 99%
“…Schwarz-like methods have also been proposed to couple dynamically distinct physics in different subdomains, for example, fluid-structure interaction, 20 and computational fluid dynamics with aero-acoustics. 21,22 Recent years have additionally seen the development of Schwarz-like methods for coupling conventional and data-driven models, including proper orthogonal decomposition (POD) reduced order models (ROMs) [23][24][25] as well as physics-informed neural networks (PINNs). 26,27 The majority of this work has focused on flow problems and steady elliptic equations, and the resulting hybrid methods are not always constructed for the purpose of multiscale coupling; for example, the main objective of the deep domain decomposition (D3M) approach proposed by Li et al 26 is to reduce the risk of over-fitting when constructing a PINN.…”
Section: Previous Workmentioning
confidence: 99%
“…The link between the two solvers CEDRE and SPACE is a two-way surfacic coupling without using a mesh overlapping contrary to what is often implemented in existing approaches [23,27,30,31]. Boundary point location and data exchange are operated via MPI communications thanks to the open source CWIPI coupling library proposed by Quemerais from ONERA [38,44].…”
Section: Coupling Proceduresmentioning
confidence: 99%
“…It suggests that two-way coupling methods need also to be investigated. Implementations of such methods can be found in the works of Borrel et al [30] or Léger et al [31] for two-dimensional and Labbé et al [32] for tri-dimensional applications with structured solvers, but tri-dimensional fully unstructured configurations are quite rare. Langenais et al [15] have carried out a two-way coupled unstructured NS-Euler computation to simulate the noise generated by an overexpanded Mach 3.1 free hot jet.…”
Section: Introductionmentioning
confidence: 99%