1990
DOI: 10.1016/0045-7930(90)90029-w
|View full text |Cite
|
Sign up to set email alerts
|

Development of a multigrid code for 3-D Navier-Stokes equations and its application to a grid-refinement study

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1
1

Citation Types

0
43
0

Year Published

1992
1992
2005
2005

Publication Types

Select...
6
2

Relationship

2
6

Authors

Journals

citations
Cited by 91 publications
(43 citation statements)
references
References 2 publications
0
43
0
Order By: Relevance
“…The equations are advanced in time with a dual time stepping scheme. A five stage RK scheme, accelerated by residual smoothing and multigrid [9,15,27], is used for advancing the solutions in pseudo-time. Second order BDF formulation is used for discretizing the physical time derivatives.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…The equations are advanced in time with a dual time stepping scheme. A five stage RK scheme, accelerated by residual smoothing and multigrid [9,15,27], is used for advancing the solutions in pseudo-time. Second order BDF formulation is used for discretizing the physical time derivatives.…”
Section: Resultsmentioning
confidence: 99%
“…Within the Jacobi preconditioning all eigenvalues are cutoff at 30% of the maximum eigenvalue. The preconditioning techniques described here have been incorporated in the TLNS3D code [27,28]. The standard TLNS3D code solves the generalized thin layer Reynolds-averaged Navier-Stokes equations, and uses residual smoothing and multigrid to accelerate the convergence to a steady state.…”
Section: Jacobi Preconditioningmentioning
confidence: 99%
“…TLNS3D, described in detail in [4], is a centraldifference code. Second-order central differences are used for all spatial derivatives, and a blend of seconddifference and fourth-difference artificial dissipation terms is used to maintain numerical stability.…”
Section: The Computer Codesmentioning
confidence: 99%
“…This paper investigates some of these issues for the studies of transonic flow over the ONERA M6 wing [1] and the Lockheed Wing C [2]. Two widely used computer codes, CFL3D [3] and TLNS3D [4], are employed. Each of these codes can employ either the Baldwin-Lomax [5] or the Johnson-King [6] turbulence model.…”
Section: Introductionmentioning
confidence: 99%
“…The TLNS3D code 16 is a high-fidelity aerodynamic computer program that solves the time-dependent three-dimensional (3-D) thin-layer Navier-Stokes equations with a finite-volume formulation.…”
Section: The Tlns3d Aerodynamic Analysis Codementioning
confidence: 99%