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Transonic flow solutions on general 3D regions using composite-block gridsThe construction of computational fluid dynamics (CFD) codes for complicated regions is greatly simplified by a composite-block grid structure since, with the use of a surrounding layer of points on each block, a flow code is then only required basically to operate on rectangular computational regions. The necessary correspondence of points on the surrounding layers (image points) with interior points (object points) is set up by the grid code and made available to the CFD solution code.
Document ID
19890058057
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thompson, Joe F.
(Mississippi State Univ. Mississippi State, MS, United States)
Whitfield, David L.
(Mississippi State University Mississippi State, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Meeting Information
Meeting: International Conference on Numerical Methods in Fluid Dynamics
Location: Williamsburg, VA
Country: United States
Start Date: June 27, 1988
End Date: July 1, 1988
Accession Number
89A45428
Funding Number(s)
CONTRACT_GRANT: NAG3-767
Distribution Limits
Public
Copyright
Other

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