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The multigrid method: Fast relaxationA multi-level grid method was studied as a possible means of accelerating convergence in relaxation calculations for transonic flows. The method employs a hierarchy of grids, ranging from very coarse (e.g. 4 x 2 mesh cells) to fine (e.g. 64 x 32); the coarser grids are used to diminish the magnitude of the smooth part of the residuals, hopefully with far less total work than would be required with optimal iterations on the finest grid. To date the method was applied quite successfully to the solution of the transonic small-disturbance equation for the velocity potential in conservation form. Nonlifting transonic flow past a parabolic arc airfoil is the example studied, with meshes of both constant and variable step size.
Document ID
19770003410
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
South, J. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Brandt, A.
(Weizmann Inst. of Sci. Rehovot, Israel)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Advan. in Eng. Sci., Vol. 4
Subject Category
Aerodynamics
Accession Number
77N10352
Funding Number(s)
CONTRACT_GRANT: NGR-47-102-001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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