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Direct control of the grid point distribution in meshes generated by elliptic equationsThe generation of computational grids suitable for obtaining accurate numerical solutions to the three-dimensional Navier-Stokes equations is the subject of intensive research. For a wide class of nozzle configurations, a three-dimensional grid can be constructed by a sequence of two-dimensional grids in successive cross-sectional planes. The present paper is concerned with numerical generation of two-dimensional grids. An effective method of interior grid control is presented based on a modified elliptic system containing free parameters. For a simply connected region, the free parameters are computed from the Dirichlet boundary values. The resulting interior grid point distribution is controlled entirely by a priori selection of the grid point distribution along the boundaries of the section.
Document ID
19790061253
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Middlecoff, J. F.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Thomas, P. D.
(Lockheed Research Laboratories Palo Alto, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 79-1462
Meeting Information
Meeting: In: Computational Fluid Dynamics Conference
Location: Williamsburg, VA
Start Date: July 23, 1979
End Date: July 25, 1979
Sponsors: Development Program, McDonnell Douglas Independent Research
Accession Number
79A45266
Funding Number(s)
CONTRACT_GRANT: NAS1-15084
Distribution Limits
Public
Copyright
Other

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