AbstractThe simulation of sound generating flows in complex geometries requires accurate numerical methods that are non-dissipative and stable, and well-posed boundary conditions. A structured mesh approach is often desired for a higher-order discretization that better uses the provided grids, but at the expense complex geometry capabilities. One solution is to use an overset mesh based discretization where locally structured meshes are globally assembled in an unstructured manner. This article discusses recent advancements in overset, also called Chimera, methods concerning boundary conditions, parallel methods for overset grid management, and stable and accurate interpolation between grids. Several examples are given, some of which includ...
The current work describes the application of high-order numerical techniques to single or multiple ...
A method for the prediction of acoustic scatter from complex geometries is presented. The discontinu...
The sound field around a finite-span airfoil subjected to a two-dimensional periodic gust is simulat...
AbstractThe simulation of sound generating flows in complex geometries requires accurate numerical m...
A high-order finite-difference algorithm is proposed in the aim of LES for Computational Aeroacousti...
Acoustic scattering from several complex geometries is simulated using a Computational AeroAcoustics...
Grid related issues of the Chimera overset grid method are discussed in the context of a method of s...
La simulation numérique des écoulements (CFD) est largement utilisée aujourd'hui dans l'industrie aé...
The direct simulation of sound sources and sound fields in flows is a rapidly growing area in resear...
Methods are presented that can be used to make multiple, overset grids communicate in a conservative...
Computational aeroacoustics requires efficient, high-resolution simulation tools. And for smooth pro...
Overset strategy can be an efficient way to keep high-accuracy discretization by decomposing a compl...
The chimera overset grid is reviewed and discussed relative to other procedures for simulating flow ...
I hereby declare that I am the sole author of this thesis. This is a true copy of the thesis, includ...
This paper presents a method to perform Navier-Stokes computations with the overset grid (or Chimera...
The current work describes the application of high-order numerical techniques to single or multiple ...
A method for the prediction of acoustic scatter from complex geometries is presented. The discontinu...
The sound field around a finite-span airfoil subjected to a two-dimensional periodic gust is simulat...
AbstractThe simulation of sound generating flows in complex geometries requires accurate numerical m...
A high-order finite-difference algorithm is proposed in the aim of LES for Computational Aeroacousti...
Acoustic scattering from several complex geometries is simulated using a Computational AeroAcoustics...
Grid related issues of the Chimera overset grid method are discussed in the context of a method of s...
La simulation numérique des écoulements (CFD) est largement utilisée aujourd'hui dans l'industrie aé...
The direct simulation of sound sources and sound fields in flows is a rapidly growing area in resear...
Methods are presented that can be used to make multiple, overset grids communicate in a conservative...
Computational aeroacoustics requires efficient, high-resolution simulation tools. And for smooth pro...
Overset strategy can be an efficient way to keep high-accuracy discretization by decomposing a compl...
The chimera overset grid is reviewed and discussed relative to other procedures for simulating flow ...
I hereby declare that I am the sole author of this thesis. This is a true copy of the thesis, includ...
This paper presents a method to perform Navier-Stokes computations with the overset grid (or Chimera...
The current work describes the application of high-order numerical techniques to single or multiple ...
A method for the prediction of acoustic scatter from complex geometries is presented. The discontinu...
The sound field around a finite-span airfoil subjected to a two-dimensional periodic gust is simulat...