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Multigrid convergence of an implicit symmetric relaxation schemeMultigrid has been applied to an existing three-dimensional compressible Euler solver to accelerate the convergence of the implicit symmetric relaxation scheme. This lower-upper symmetric Gauss-Seidel implicit scheme is shown to be an effective multigrid driver in three-dimensions. A grid refinement study is performed including the effects of large cell aspect ratio meshes. Performance figures of the present multigrid code on Cray computers including the new C90 are presented. A reduction of three orders of of magnitude in the residual for a three-dimensional transonic inviscid flow using 920K grid points is obtained in less than 4 minutes on a Cray C90.
Document ID
19930061054
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yoon, Seokkwan
(NASA Ames Research Center Moffett Field, CA, United States)
Chang, Leon
(MCAT Inst. Moffett Field, CA, United States)
Kwak, Dochan
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Computational Fluid Dynamics Conference, 11th, Orlando, FL, July 6-9, 1993, Technical Papers. Pt. 2 (A93-44994 18-34)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-3357
Accession Number
93A45051
Distribution Limits
Public
Copyright
Other

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