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Multistage Schemes with Multigrid for Euler and Navier-Strokes Equations: Components and AnalysisA class of explicit multistage time-stepping schemes with centered spatial differencing and multigrids are considered for the compressible Euler and Navier-Stokes equations. These schemes are the basis for a family of computer programs (flow codes with multigrid (FLOMG) series) currently used to solve a wide range of fluid dynamics problems, including internal and external flows. In this paper, the components of these multistage time-stepping schemes are defined, discussed, and in many cases analyzed to provide additional insight into their behavior. Special emphasis is given to numerical dissipation, stability of Runge-Kutta schemes, and the convergence acceleration techniques of multigrid and implicit residual smoothing. Both the Baldwin and Lomax algebraic equilibrium model and the Johnson and King one-half equation nonequilibrium model are used to establish turbulence closure. Implementation of these models is described.
Document ID
19970028360
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Swanson, R. C.
(NASA Langley Research Center Hampton, VA United States)
Turkel, Eli
(Tel-Aviv Univ., Ramat-Aviv Tel-Aviv, Israel)
Date Acquired
September 6, 2013
Publication Date
August 1, 1997
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.60:3631
L-17201
NASA-TP-3631
Report Number: NAS 1.60:3631
Report Number: L-17201
Report Number: NASA-TP-3631
Accession Number
97N27148
Funding Number(s)
PROJECT: RTOP 505-59-53-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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