We describe an approach to simulate accurately viscous flows around complex configurations using overset grids. A combination of patched multi-block and overlapping grids is used to discretize the flow domain. A hierarchical grid system with different layers of grids of varying resolution ensures inter-grid connectivity within a multigrid solution acceleration framework. At each stage of the numerical computation, the block boundaries maintain a regular information exchange between neighboring blocks be it patched or overlapping boundaries. Coarse-grain parallel processing is facilitated by the multi-blocking system. Numerical results of flows over multi-element airfoils and three-dimensional turbulent flows around wing-body aerodynamic con...
A general proof-of-concept prototype multiblock system, which provides Euler and Navier-Stokes flow ...
AbstractIn the design process of rocket, airplane and store separation systems, the aerodynamic of m...
This paper briefly addresses the computational requirements for the analysis of complete configurati...
grantor: University of TorontoA multigrid algorithm to accelerate the convergence of the c...
This paper explores the parallel performance of structured overset CFD computations for multicompone...
The multi-block overset grid method is a powerful technique for high-fidelity computational fluid dy...
In this user`s guide, details for running BREAKUP are discussed. BREAKUP allows the widely used over...
The paper discusses the combined implementation of overset grid and patched grid methodologies and i...
The overset grid methodology has significantly reduced time-to-solution of highfidelity computationa...
A simple, robust numerical algorithm to localize intergrid boundary points and to interpolate unstea...
The goal of this study involves developing an efficient and accurate parallel computation method for...
Collection of Technical Papers - 22nd AIAA Applied Aerodynamics Conference1603-62
Analysis of modern aerospace vehicles requires the computation of flowfields about complex three dim...
Grid related issues of the Chimera overset grid method are discussed in the context of a method of s...
The development and testing of a parallel unstructured agglomeration multigrid algorithm for steady-...
A general proof-of-concept prototype multiblock system, which provides Euler and Navier-Stokes flow ...
AbstractIn the design process of rocket, airplane and store separation systems, the aerodynamic of m...
This paper briefly addresses the computational requirements for the analysis of complete configurati...
grantor: University of TorontoA multigrid algorithm to accelerate the convergence of the c...
This paper explores the parallel performance of structured overset CFD computations for multicompone...
The multi-block overset grid method is a powerful technique for high-fidelity computational fluid dy...
In this user`s guide, details for running BREAKUP are discussed. BREAKUP allows the widely used over...
The paper discusses the combined implementation of overset grid and patched grid methodologies and i...
The overset grid methodology has significantly reduced time-to-solution of highfidelity computationa...
A simple, robust numerical algorithm to localize intergrid boundary points and to interpolate unstea...
The goal of this study involves developing an efficient and accurate parallel computation method for...
Collection of Technical Papers - 22nd AIAA Applied Aerodynamics Conference1603-62
Analysis of modern aerospace vehicles requires the computation of flowfields about complex three dim...
Grid related issues of the Chimera overset grid method are discussed in the context of a method of s...
The development and testing of a parallel unstructured agglomeration multigrid algorithm for steady-...
A general proof-of-concept prototype multiblock system, which provides Euler and Navier-Stokes flow ...
AbstractIn the design process of rocket, airplane and store separation systems, the aerodynamic of m...
This paper briefly addresses the computational requirements for the analysis of complete configurati...