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Comparison of three explicit multigrid methods for the Euler and Navier-Stokes equationsThree explicit multigrid methods, Ni's method, Jameson's finite-volume method, and a finite-difference method based on Brandt's work, are described and compared for two model problems. All three methods use an explicit multistage Runge-Kutta scheme on the fine grid, and this scheme is also described. Convergence histories for inviscid flow over a bump in a channel for the fine-grid scheme alone show that convergence rate is proportional to Courant number and that implicit residual smoothing can significantly accelerate the scheme. Ni's method was slightly slower than the implicitly-smoothed scheme alone. Brandt's and Jameson's methods are shown to be equivalent in form but differ in their node versus cell-centered implementations. They are about 8.5 times faster than Ni's method in terms of CPU time. Results for an oblique shock/boundary layer interaction problem verify the accuracy of the finite-difference code. All methods slowed considerably on the stretched viscous grid but Brandt's method was still 2.1 times faster than Ni's method.
Document ID
19870007351
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chima, Rodrick V.
(NASA Lewis Research Center Cleveland, OH, United States)
Turkel, Eli
(NASA Lewis Research Center Cleveland, OH, United States)
Schaffer, Steve
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:88878
E-3126
ICOMP-86-3
NASA-TM-88878
Report Number: NAS 1.15:88878
Report Number: E-3126
Report Number: ICOMP-86-3
Report Number: NASA-TM-88878
Accession Number
87N16784
Funding Number(s)
PROJECT: RTOP 505-31-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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