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Convergence of Defect-Correction and Multigrid Iterations for Inviscid FlowsConvergence of multigrid and defect-correction iterations is comprehensively studied within different incompressible and compressible inviscid regimes on high-density grids. Good smoothing properties of the defect-correction relaxation have been shown using both a modified Fourier analysis and a more general idealized-coarse-grid analysis. Single-grid defect correction alone has some slowly converging iterations on grids of medium density. The convergence is especially slow for near-sonic flows and for very low compressible Mach numbers. Additionally, the fast asymptotic convergence seen on medium density grids deteriorates on high-density grids. Certain downstream-boundary modes are very slowly damped on high-density grids. Multigrid scheme accelerates convergence of the slow defect-correction iterations to the extent determined by the coarse-grid correction. The two-level asymptotic convergence rates are stable and significantly below one in most of the regions but slow convergence is noted for near-sonic and very low-Mach compressible flows. Multigrid solver has been applied to the NACA 0012 airfoil and to different flow regimes, such as near-tangency and stagnation. Certain convergence difficulties have been encountered within stagnation regions. Nonetheless, for the airfoil flow, with a sharp trailing-edge, residuals were fast converging for a subcritical flow on a sequence of grids. For supercritical flow, residuals converged slower on some intermediate grids than on the finest grid or the two coarsest grids.
Document ID
20110013655
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Diskin, Boris
(National Inst. of Aerospace Hampton, VA, United States)
Thomas, James L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
June 27, 2011
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-11822
AIAA Paper 2011-3235
Report Number: NF1676L-11822
Report Number: AIAA Paper 2011-3235
Meeting Information
Meeting: 41st AIAA Fluid Dynamics Conference and Exhibit
Location: Honolulu, HI
Country: United States
Start Date: June 27, 2011
End Date: June 30, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNL07AA23C
WBS: WBS 561581.02.07.07.20
Distribution Limits
Public
Copyright
Public Use Permitted.
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