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An Initial Investigation of the Effects of Turbulence Models on the Convergence of the RK/Implicit SchemeA three-stage Runge-Kutta (RK) scheme with multigrid and an implicit preconditioner has been shown to be an effective solver for the fluid dynamic equations. This scheme has been applied to both the compressible and essentially incompressible Reynolds-averaged Navier-Stokes (RANS) equations using the algebraic turbulence model of Baldwin and Lomax (BL). In this paper we focus on the convergence of the RK/implicit scheme when the effects of turbulence are represented by either the Spalart-Allmaras model or the Wilcox k-! model, which are frequently used models in practical fluid dynamic applications. Convergence behavior of the scheme with these turbulence models and the BL model are directly compared. For this initial investigation we solve the flow equations and the partial differential equations of the turbulence models indirectly coupled. With this approach we examine the convergence behavior of each system. Both point and line symmetric Gauss-Seidel are considered for approximating the inverse of the implicit operator of the flow solver. To solve the turbulence equations we use a diagonally dominant alternating direction implicit (DDADI) scheme. Computational results are presented for three airfoil flow cases and comparisons are made with experimental data. We demonstrate that the two-dimensional RANS equations and transport-type equations for turbulence modeling can be efficiently solved with an indirectly coupled algorithm that uses the RK/implicit scheme for the flow equations.
Document ID
20080041600
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Swanson, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Rossow, C.-C.
(Deutsches Zentrum fuer Luft- und Raumfahrt e.V. Braunschweig, Germany)
Date Acquired
August 24, 2013
Publication Date
August 1, 2008
Subject Category
Numerical Analysis
Report/Patent Number
NASA/TM-2008-215342
L-19509
Report Number: NASA/TM-2008-215342
Report Number: L-19509
Funding Number(s)
WBS: WBS 561581.02.08.07.20.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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