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A study of dissipation operators for the euler equations and a three- dimensional channel flow

Published: 01 August 1989 Publication History

Abstract

Explicit methods for the solution of fluid flow problems are of considerable interest in supercomputing. These methods parallelize well. The treatment of the boundaries is of particular interest both with respect to the numeric behavior of the solution, and the computational efficiency. We have solved the three-dimensional Euler equations for a twisted channel using second-order, centered difference operators, and a three stage Runge-Kutta method for the integration. Three different fourth-order dissipation operators were studied for numeric stabilization: one positive definite, [8], one positive semidefinite, [3], and one indefinite. The operators only differ in the treatment of the boundary. For computational efficiency all dissipation operators were designed with a constant bandwidth in matrix representation, with the bandwidth determined by the operator in the interior. The positive definite dissipation operator results in a significant growth in entropy close to the channel walls. The other operators maintain constant entropy.
Several different implementations of the semidefinite operator obtained through factoring of the operator were also studied. We show the difference both in convergence rate and robustness for the different dissipation operators, and the factorizations of the operator due to Eriksson. For the simulations in this study one of the factorizations of the semidefinite operator required 70 - 90% of the number of iterations required by the positive definite operator. The indefinite operator was sensitive to perturbations in the inflow boundary conditions. The simulations were performed on a 8,192 processor Connection Machine system model CM-2. Full processor utilization was achieved, and a performance of 135 Mflops/s in single precision was obtained. A performance of 1.1 Gflops/s for a fully configured system with 65,536 processors was demonstrated.

References

[1]
R. Courant and K. O. Friedrichs. Supersonic Flow and Shock Waves, volume I of Pure and Applied Mathematics. Interscience Publishers, Inc., New York, 1948.
[2]
Rickard Enander and Johan Sowa. Numerical simulation of fluid flow in a twisted channel. Technical Report 88-01, Department of Scienti~c Computing, Uppsala University, 1988.
[3]
L. E. Eriksson. Boundary conditions for artificial dissipation operators. Technical Report FFA TN 1984-53, The Aeronautical Research Institute of Sweden, Aerodynamics Department, Stockholm, Sweden, 1984.
[4]
A. 3ameson, W. Schmidt, and E. Turkel. Numerical solutions of the Euler equations by finite volume methods using Kunge-Kutta time-stepping schemes. AIAA Paper, 81-1259, 1981.
[5]
S. Lennart Johnsson. Future high performance computation: The megaflop per dollar alternative. Technical Report YALEU/DCS/RR-360, Dept. of Computer Science, Yale University, January 1985.
[6]
Pelle Olsson and S. Lennart Johnsson. A dataparallel implementation of explicit methods for the threedimensional compressible Navier-Stokes equations. Technical Report CS-89/4, Thinking Machines Corp., February 1989.
[7]
Pelle Olsson and S. Lennart Johnsson. A study of dissipation operators for the Euler equations and threedimensional channel flow. Technical Report CS-89/3, Thinking Machines Corp., February 1989.
[8]
Thomas E Pulliam. Artificial dissipation models for the Euler equations. AIAA, 24(12), December 1986.

Cited By

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  • (2012)A High-Order Parallel Newton-Krylov Flow Solver for the Euler Equations19th AIAA Computational Fluid Dynamics10.2514/6.2009-3657Online publication date: 14-Jun-2012

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cover image ACM Conferences
Supercomputing '89: Proceedings of the 1989 ACM/IEEE conference on Supercomputing
August 1989
849 pages
ISBN:0897913418
DOI:10.1145/76263
Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]

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  • Los Alamos National Labs: Los Alamos National Labs
  • NASA: National Aeronatics and Space Administration
  • Argonne Natl Lab: Argonne National Lab

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Association for Computing Machinery

New York, NY, United States

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Published: 01 August 1989

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  • (2012)A High-Order Parallel Newton-Krylov Flow Solver for the Euler Equations19th AIAA Computational Fluid Dynamics10.2514/6.2009-3657Online publication date: 14-Jun-2012

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