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A Multiple-Block Multigrid Method for the Solution of the Three-Dimensional Euler and Navier-Stokes Equations.

Atkins, H. (1990) A Multiple-Block Multigrid Method for the Solution of the Three-Dimensional Euler and Navier-Stokes Equations. DLR-Forschungsbericht. 90-45. 27 S.

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Abstract

A multiple multigrid method for the solution of the 3-D Euler and Navier-Stokes equations is presented. The basic flow solver is a cell-vertex method which employs central difference spatial approximations and Runge-Kutta time stepping. The use of local time stepping, implicit residual smoothing, multigrid techniques and variable-coefficient numerical dissipation results in an efficient and robust scheme. The multi-block calculations in which the two-block grid is generated by splitting the one-block grid. Results are presented for both Euler and Navier-Stokes computations of wings and wing/fuselage combinations.

Item URL in elib:https://elib.dlr.de/35777/
Document Type:Monograph (DLR-Forschungsbericht)
Additional Information: LIDO-Berichtsjahr=1990,
Title:A Multiple-Block Multigrid Method for the Solution of the Three-Dimensional Euler and Navier-Stokes Equations.
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Atkins, H.NASA-Langley Research Center, Hampton, Va.UNSPECIFIEDUNSPECIFIED
Date:1990
Open Access:No
Number of Pages:27
Status:Published
Keywords:Multiple Block, Multigrid, Runge-Kutta Scheme, Euler Equations, Navier-Stokes Equations
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:no assignment
DLR - Research theme (Project):L - Concepts & Integration (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik
Deposited By: DLR-Beauftragter, elib
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:04

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