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Near-Body Grid Adaption for Overset GridsA solution adaption capability for curvilinear near-body grids has been implemented in the OVERFLOW overset grid computational fluid dynamics code. The approach follows closely that used for the Cartesian off-body grids, but inserts refined grids in the computational space of original near-body grids. Refined curvilinear grids are generated using parametric cubic interpolation, with one-sided biasing based on curvature and stretching ratio of the original grid. Sensor functions, grid marking, and solution interpolation tasks are implemented in the same fashion as for off-body grids. A goal-oriented procedure, based on largest error first, is included for controlling growth rate and maximum size of the adapted grid system. The adaption process is almost entirely parallelized using MPI, resulting in a capability suitable for viscous, moving body simulations. Two- and three-dimensional examples are presented.
Document ID
20160010116
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Buning, Pieter G.
(NASA Langley Research Center Hampton, VA, United States)
Pulliam, Thomas H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 5, 2016
Publication Date
June 13, 2016
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-22810
Report Number: NF1676L-22810
Meeting Information
Meeting: AIAA Aviation 2016
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 664817.02.07.04.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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