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The Development of a Factorizable Multigrid Algorithm for Subsonic and Transonic FlowThe factorizable discretization of Sidilkover for the compressible Euler equations previously demonstrated for channel flows has been extended to external flows.The dissipation of the original scheme has been modified to maintain stability for moderately stretched grids. The discrete equations are solved by symmetric collective Gauss-Seidel relaxation and FAS multigrid. Unlike the earlier work ordering the grid vertices in the flow direction has been found to be unnecessary. Solutions for essential incompressible flow (Mach 0.01) and supercritical flows have obtained for a Karman-Trefftz airfoil with it conformally mapped grid,as well as a NACA 0012 on an algebraically generated grid. The current work demonstrates nearly 0(n) convergence for subsonic and slightly transonic flows.
Document ID
20010051653
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Roberts, Thomas W.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2001-2572
Report Number: AIAA Paper 2001-2572
Meeting Information
Meeting: 15th AIAA Computational Fluid Dynamics Conference
Location: Anaheim, CA
Country: United States
Start Date: June 11, 2001
End Date: June 14, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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