NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A barely implicit correction for flux-corrected transportIn virtue of adding one elliptic equation that must be implicitly solved, the 'barely implicit correction' method presented removes the stringent sidestep limit imposed by sound speed in the explicit methods. The barely implicit method is presently combined with a flux-corrected transport algorithm, which has been rendered fourth-order by the appropriate subtraction of corrected fluxes, in order to accurately represent the sharp gradients in subsonic flows. The multigrid MGRID technique (DeVore, 1984) is used to efficiently solve the elliptic pressure equation.
Document ID
19870057719
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Patnaik, G.
(Naval Research Lab. Washington, DC, United States)
Guirguis, R. H.
(Naval Research Lab. Washington, DC, United States)
Boris, J. P.
(Naval Research Lab. Washington, DC, United States)
Oran, E. S.
(U.S. Navy, Naval Research Laboratory, Washington DC, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1987
Publication Information
Publication: Journal of Computational Physics
Volume: 71
ISSN: 0021-9991
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ISSN: 0021-9991
Accession Number
87A44993
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available