This paper explores the parallel performance of structured overset CFD computations for multicomponent bodies in which there is relative motion between component parts. The two processes that dominate the cost of such problems are the flow solution on each component and the intergrid connectivity solution. A two-part static-dynamic load balancing scheme is proposed in which the static part balances the load for the flow solution and the dynamic part re-balances, if necessary, the load for the connectivity solution. This scheme is coupled with existing parallel implementations of the OVERFLOW flow solver and DCF3D connectivity routine and used for unsteady calculations about aerodynamic bodies on the IBM SP2 and IBM SP multi-processors. This...
In the computational fluid dynamic simulation of problems with complex geometries or multiscale spat...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
Analysis of modern aerospace vehicles requires the computation of flowfields about complex three dim...
We describe an approach to simulate accurately viscous flows around complex configurations using ove...
The multi-block overset grid method is a powerful technique for high-fidelity computational fluid dy...
The overset grid methodology has significantly reduced time-to-solution of highfidelity computationa...
The goal of this study involves developing an efficient and accurate parallel computation method for...
This paper describes the parallelization of a dynamic overset grid approach with predefined holes. T...
AbstractIn the design process of rocket, airplane and store separation systems, the aerodynamic of m...
In this user`s guide, details for running BREAKUP are discussed. BREAKUP allows the widely used over...
Aerodynamic problems involving moving objects have many applications, including store separation, fl...
The paper discusses the combined implementation of overset grid and patched grid methodologies and i...
In this paper we present the parallel version of a CFD solver which works on unstructured 3-dimensio...
A discussion of the strengths and weaknesses of overset composite grid and solution technology is gi...
University of Minnesota Ph.D. dissertation. December 2018. Major: Aerospace Engineering and Mechanic...
In the computational fluid dynamic simulation of problems with complex geometries or multiscale spat...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
Analysis of modern aerospace vehicles requires the computation of flowfields about complex three dim...
We describe an approach to simulate accurately viscous flows around complex configurations using ove...
The multi-block overset grid method is a powerful technique for high-fidelity computational fluid dy...
The overset grid methodology has significantly reduced time-to-solution of highfidelity computationa...
The goal of this study involves developing an efficient and accurate parallel computation method for...
This paper describes the parallelization of a dynamic overset grid approach with predefined holes. T...
AbstractIn the design process of rocket, airplane and store separation systems, the aerodynamic of m...
In this user`s guide, details for running BREAKUP are discussed. BREAKUP allows the widely used over...
Aerodynamic problems involving moving objects have many applications, including store separation, fl...
The paper discusses the combined implementation of overset grid and patched grid methodologies and i...
In this paper we present the parallel version of a CFD solver which works on unstructured 3-dimensio...
A discussion of the strengths and weaknesses of overset composite grid and solution technology is gi...
University of Minnesota Ph.D. dissertation. December 2018. Major: Aerospace Engineering and Mechanic...
In the computational fluid dynamic simulation of problems with complex geometries or multiscale spat...
A deformable overset grid method was proposed to simulate the unsteady aerodynamic problems with mu...
Analysis of modern aerospace vehicles requires the computation of flowfields about complex three dim...