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A locally refined rectangular grid finite element method - Application to computational fluid dynamics and computational physicsThe present FEM technique addresses both linear and nonlinear boundary value problems encountered in computational physics by handling general three-dimensional regions, boundary conditions, and material properties. The box finite elements used are defined by a Cartesian grid independent of the boundary definition, and local refinements proceed by dividing a given box element into eight subelements. Discretization employs trilinear approximations on the box elements; special element stiffness matrices are included for boxes cut by any boundary surface. Illustrative results are presented for representative aerodynamics problems involving up to 400,000 elements.
Document ID
19910037655
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Young, David P.
(Boeing Computer Services Co. Seattle, WA, United States)
Melvin, Robin G.
(Boeing Computer Services Co. Seattle, WA, United States)
Bieterman, Michael B.
(Boeing Computer Services Seattle, WA, United States)
Johnson, Forrester T.
(Boeing Computer Services Co. Seattle, WA, United States)
Samant, Satish S.
(Boeing Commercial Airplanes Seattle, WA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: Journal of Computational Physics
Volume: 92
ISSN: 0021-9991
Subject Category
Numerical Analysis
Accession Number
91A22278
Funding Number(s)
CONTRACT_GRANT: NAS2-12513
Distribution Limits
Public
Copyright
Other

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