NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A Cartesian grid approach with hierarchical refinement for compressible flowsMany numerical studies of flows that involve complex geometries are limited by the difficulties in generating suitable grids. We present a Cartesian boundary scheme for two-dimensional, compressible flows that is unfettered by the need to generate a computational grid and so it may be used, routinely, even for the most awkward of geometries. In essence, an arbitrary-shaped body is allowed to blank out some region of a background Cartesian mesh and the resultant cut-cells are singled out for special treatment. This is done within a finite-volume framework and so, in principle, any explicit flux-based integration scheme can take advantage of this method for enforcing solid boundary conditions. For best effect, the present Cartesian boundary scheme has been combined with a sophisticated, local mesh refinement scheme, and a number of examples are shown in order to demonstrate the efficacy of the combined algorithm for simulations of shock interaction phenomena.
Document ID
19950004530
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Quirk, James J.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Numerical Analysis
Report/Patent Number
ICASE-94-51
NAS 1.26:194938
NASA-CR-194938
AD-A285080
Report Number: ICASE-94-51
Report Number: NAS 1.26:194938
Report Number: NASA-CR-194938
Report Number: AD-A285080
Meeting Information
Meeting: European Computational Mechanics Symposium
Start Date: January 1, 1995
Accession Number
95N10943
Funding Number(s)
CONTRACT_GRANT: NAS1-19480
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available