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Error Reduction ProgramThe details of a study to select, incorporate and evaluate the best available finite difference scheme to reduce numerical error in combustor performance evaluation codes are described. The combustor performance computer programs chosen were the two dimensional and three dimensional versions of Pratt & Whitney's TEACH code. The criteria used to select schemes required that the difference equations mirror the properties of the governing differential equation, be more accurate than the current hybrid difference scheme, be stable and economical, be compatible with TEACH codes, use only modest amounts of additional storage, and be relatively simple. The methods of assessment used in the selection process consisted of examination of the difference equation, evaluation of the properties of the coefficient matrix, Taylor series analysis, and performance on model problems. Five schemes from the literature and three schemes developed during the course of the study were evaluated. This effort resulted in the incorporation of a scheme in 3D-TEACH which is usuallly more accurate than the hybrid differencing method and never less accurate.
Document ID
19850019273
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Syed, S. A.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Chiappetta, L. M.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Gosman, A. D.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 5, 2013
Publication Date
January 11, 1985
Subject Category
Numerical Analysis
Report/Patent Number
NAS 1.26:174776
NASA-CR-174776
PWA-5928-25
Report Number: NAS 1.26:174776
Report Number: NASA-CR-174776
Report Number: PWA-5928-25
Accession Number
85N27584
Funding Number(s)
CONTRACT_GRANT: NAS3-23686
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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