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Reducing numerical diffusion for incompressible flow calculationsA number of approaches for improving the accuracy of incompressible, steady-state flow calculations are examined. Two improved differencing schemes, Quadratic Upstream Interpolation for Convective Kinematics (QUICK) and Skew-Upwind Differencing (SUD), are applied to the convective terms in the Navier-Stokes equations and compared with results obtained using hybrid differencing. In a number of test calculations, it is illustrated that no single scheme exhibits superior performance for all flow situations. However, both SUD and QUICK are shown to be generally more accurate than hybrid differencing.
Document ID
19850006531
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Claus, R. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Neely, G. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Syed, S. A.
(United Technologies East Hartford, Conn., United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-2055
NASA-TM-83621
NAS 1.15:83621
Report Number: E-2055
Report Number: NASA-TM-83621
Report Number: NAS 1.15:83621
Meeting Information
Meeting: Western States Meeting of the Combustion Inst.
Location: Boulder, CO
Country: United States
Start Date: April 2, 1984
End Date: April 3, 1984
Accession Number
85N14840
Funding Number(s)
PROJECT: RTOP 505-31-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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