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Numerical solution of potential flow about arbitrary 2-dimensional multiple bodiesA procedure for the finite-difference numerical solution of the lifting potential flow about any number of arbitrarily shaped bodies is given. The solution is based on a technique of automatic numerical generation of a curvilinear coordinate system having coordinate lines coincident with the contours of all bodies in the field, regardless of their shapes and number. The effects of all numerical parameters involved are analyzed and appropriate values are recommended. Comparisons with analytic solutions for single Karman-Trefftz airfoils and a circular cylinder pair show excellent agreement. The technique of application of the boundary-fitted coordinate systems to the numerical solution of partial differential equations is illustrated.
Document ID
19820015596
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Thompson, J. F.
(Mississippi State Univ. Hampton, VA, United States)
Thames, F. C.
(NASA Langley Research Center)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
MSSU-EIRS-ASE-82-2
NASA-TM-84737
NAS 1.15:84737
Report Number: MSSU-EIRS-ASE-82-2
Report Number: NASA-TM-84737
Report Number: NAS 1.15:84737
Accession Number
82N23470
Funding Number(s)
CONTRACT_GRANT: NGR-25-001-055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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