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An alternative to unstructured grids for computing gas dynamic flows around arbitrarily complex two-dimensional bodiesIn this paper we describe an approach for dealing with arbitrary complex, two dimensional geometries, the so-called cartesian boundary method. Conceptually, the cartesian boundary method is quite simple. Solid bodies blank out areas of a background, cartesian mesh, and the resultant cut cells are singled out for special attention. However, there are several obstacles that must be overcome in order to achieve a practical scheme. We present a general strategy that overcomes these obstacles, together with some details of our successful conversion of an adaptive mesh algorithm from a body-fitted code to a cartesian boundary code.
Document ID
19920012222
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Quirk, James J.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
ICASE-92-7
NASA-CR-189612
AD-A248783
NAS 1.26:189612
Report Number: ICASE-92-7
Report Number: NASA-CR-189612
Report Number: AD-A248783
Report Number: NAS 1.26:189612
Accession Number
92N21465
Funding Number(s)
CONTRACT_GRANT: NAS1-18605
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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