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Error reduction program: A progress reportFive finite differences schemes were evaluated for minimum numerical diffusion in an effort to identify and incorporate the best error reduction scheme into a 3D combustor performance code. Based on this evaluated, two finite volume method schemes were selected for further study. Both the quadratic upstream differencing scheme (QUDS) and the bounded skew upstream differencing scheme two (BSUDS2) were coded into a two dimensional computer code and their accuracy and stability determined by running several test cases. It was found that BSUDS2 was more stable than QUDS. It was also found that the accuracy of both schemes is dependent on the angle that the streamline make with the mesh with QUDS being more accurate at smaller angles and BSUDS2 more accurate at larger angles. The BSUDS2 scheme was selected for extension into three dimensions.
Document ID
19840012468
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Syed, S. A.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Aircraft Propulsion And Power
Accession Number
84N20536
Funding Number(s)
CONTRACT_GRANT: NAS3-23686
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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