We study the computational, communication, and scalability characteristics of a computational fluid dynamics application, which solves the time accurate flow field of a jet using the compressible Navier-Stokes equations, on a variety of parallel architecture platforms. The platforms chosen for this study are a cluster of workstations (the LACE experimental testbed at NASA Lewis), a shared memory multiprocessor (the Cray YMP), and distributed memory multiprocessors with different topologies - the IBM SP and the Cray T3D. We investigate the impact of various networks connecting the cluster of workstations on the performance of the application and the overheads induced by popular message passing libraries used for parallelization. The work als...
In this paper we discuss and demonstrate the feasibility of solving high-fidelity, nonlinear computa...
We are surveying current projects in the area of parallel supercomputers. The machines considered he...
The current computing environment that most researchers are using for the calculation of 3D unsteady...
We study the computational, communication, and scalability characteristics of a Computational Fluid ...
We study the computational, communication, and scalability characteristics of a Computational Fluid ...
The results of the implementation of a Navier-Stokes algorithm on three parallel/vector computers ar...
Phase 1 is complete for the development of a computational fluid dynamics CFD) parallel code with au...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76255/1/AIAA-1989-1940-323.pd
The results of an experiment are reported, i.c., to adapt a Navier-Stokes code, originally developed...
The Numerical Aerodynamic Simulation (NAS) Program, which is based at NASA Ames Research Center, is ...
The ALLSPD-3D Computational Fluid Dynamics code for reacting flow simulation was run on a set of ben...
The parallel execution of an aerodynamic simulation code on a non-dedicated, heterogeneous cluster ...
An explicit flow solver, applicable to the hierarchy of model equations ranging from Euler to full N...
A new set of benchmarks was developed for the performance evaluation of highly parallel supercompute...
Some existing parallel N-S codes, including both explicit and implicit algorithms, have been ported ...
In this paper we discuss and demonstrate the feasibility of solving high-fidelity, nonlinear computa...
We are surveying current projects in the area of parallel supercomputers. The machines considered he...
The current computing environment that most researchers are using for the calculation of 3D unsteady...
We study the computational, communication, and scalability characteristics of a Computational Fluid ...
We study the computational, communication, and scalability characteristics of a Computational Fluid ...
The results of the implementation of a Navier-Stokes algorithm on three parallel/vector computers ar...
Phase 1 is complete for the development of a computational fluid dynamics CFD) parallel code with au...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76255/1/AIAA-1989-1940-323.pd
The results of an experiment are reported, i.c., to adapt a Navier-Stokes code, originally developed...
The Numerical Aerodynamic Simulation (NAS) Program, which is based at NASA Ames Research Center, is ...
The ALLSPD-3D Computational Fluid Dynamics code for reacting flow simulation was run on a set of ben...
The parallel execution of an aerodynamic simulation code on a non-dedicated, heterogeneous cluster ...
An explicit flow solver, applicable to the hierarchy of model equations ranging from Euler to full N...
A new set of benchmarks was developed for the performance evaluation of highly parallel supercompute...
Some existing parallel N-S codes, including both explicit and implicit algorithms, have been ported ...
In this paper we discuss and demonstrate the feasibility of solving high-fidelity, nonlinear computa...
We are surveying current projects in the area of parallel supercomputers. The machines considered he...
The current computing environment that most researchers are using for the calculation of 3D unsteady...