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Grid flexibility and patching techniquesThe numerical determination of combustor flowfields is of great value to the combustor designer. An a priori knowledge of the flow behavior can speed the combustor design process and reduce the number of experimental test rigs required to arrive at an optimal design. Even 2-D steady incompressible isothermal flow predictions are of use; many codes of this kind are available, each employing different techniques to surmount the difficulties arising from the nonlinearity of the governing equations and from typically irregular combustor geometries. Mapping techniques (algebraic and elliptic PDE), and adaptive grid methods (both multi-grid and grid embedding) as applied to axisymmetric combustors are discussed.
Document ID
19840012472
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Keith, T. G.
(Toledo Univ. OH, United States)
Smith, L. W.
(Toledo Univ. OH, United States)
Yung, C. N.
(Toledo Univ. OH, United States)
Barthelson, S. H.
(Toledo Univ. OH, United States)
Dewitt, K. J.
(Toledo Univ. OH, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Numerical Analysis
Accession Number
84N20540
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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