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Accuracy enhancements for overset grids using a defect correction approachA defect-correction approach is investigated as a means of enhancing the accuracy of flow computations on overset grids. Typically, overset-grid techniques process and pass information only at grid boundaries. In the current approach, error corrections at all overlapped interior points are injected between grids by using a defect-correction scheme. In some cases this is found to enhance the overall accuracy of the overset-grid method. Locally refined overset grids can be used to provide an efficient solution-adaptation method. The defect correction can also be ultilized as an error-correction technique for a coarse grid by evaluating the residual using a fine base grid, but solving the implicit equations only on the coarse grid. Numerical examples include an accuracy and dissipation study of an unsteady decaying vortex flow, the flow over a NACA 0012 airfoil, and the flow over a mulit-element high-lift airfoil.
Document ID
19950028582
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rogers, Stuart E.
(NASA Ames Research Center Moffett Field, CA, United States)
Pulliam, Thomas H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 16, 2013
Publication Date
January 10, 1994
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 94-0523
Accession Number
95A60181
Distribution Limits
Public
Copyright
Other

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