A technique allowing time-staggered solution of partial differential equations is presented in this report. Using this technique, called time-partitioning, simulation execution speedup is proportional to the number of processors used because all processors operate simultaneously, with each updating of the solution grid at a different time point. The technique is limited by neither the number of processors available nor by the dimension of the solution grid. Time-partitioning was used to obtain the flow pattern through a cascade of airfoils, modeled by the Euler partial differential equations. An execution speedup factor of 1.77 was achieved using a two processor Cray X-MP/24 computer
An explicit flow solver, applicable to the hierarchy of model equations ranging from Euler to full N...
The co-simulation methods considered here are based on the idea of splitting an overall model into d...
The size of the output originating from large scale, numerical simulations poses major bottlenecks i...
The development of multiprocessor simulations from a serial set of ordinary differential equations d...
The development of numerical methods and software tools for parallel processors can be aided through...
A FORTRAN program describing the vibration modes of a rotor-bearing system is analyzed for parelleli...
The Navier-Stokes Computer is a multi-purpose parallel-processing supercomputer which is currently u...
Phase I is complete for the development of a Computational Fluid Dynamics parallel code with automat...
Phase 1 is complete for the development of a computational fluid dynamics CFD) parallel code with au...
The NASA Lewis Research Center is actively involved in the development of expert system technology t...
Very little use is made of multiple processors available on current supercomputers (computers with a...
This chapter is focused on creation, accuracy, and simulation of two-parameter control of a mathemat...
This chapter is focused on creation, accuracy, and simulation of two-parameter control of a mathemat...
The parallel execution of an aerodynamic simulation code on a non-dedicated, heterogeneous cluster ...
We present a reformulation of unsteady turbulent flow simulations. The initial condition is relaxed ...
An explicit flow solver, applicable to the hierarchy of model equations ranging from Euler to full N...
The co-simulation methods considered here are based on the idea of splitting an overall model into d...
The size of the output originating from large scale, numerical simulations poses major bottlenecks i...
The development of multiprocessor simulations from a serial set of ordinary differential equations d...
The development of numerical methods and software tools for parallel processors can be aided through...
A FORTRAN program describing the vibration modes of a rotor-bearing system is analyzed for parelleli...
The Navier-Stokes Computer is a multi-purpose parallel-processing supercomputer which is currently u...
Phase I is complete for the development of a Computational Fluid Dynamics parallel code with automat...
Phase 1 is complete for the development of a computational fluid dynamics CFD) parallel code with au...
The NASA Lewis Research Center is actively involved in the development of expert system technology t...
Very little use is made of multiple processors available on current supercomputers (computers with a...
This chapter is focused on creation, accuracy, and simulation of two-parameter control of a mathemat...
This chapter is focused on creation, accuracy, and simulation of two-parameter control of a mathemat...
The parallel execution of an aerodynamic simulation code on a non-dedicated, heterogeneous cluster ...
We present a reformulation of unsteady turbulent flow simulations. The initial condition is relaxed ...
An explicit flow solver, applicable to the hierarchy of model equations ranging from Euler to full N...
The co-simulation methods considered here are based on the idea of splitting an overall model into d...
The size of the output originating from large scale, numerical simulations poses major bottlenecks i...