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Accelerated convergence for incompressible flow calculationsTwo improved algorithms which solve the steady-state Navier-Stokes equations, PISO and SIMPLER, are studied. Computations were carried out on progressively finer grids for the driven cavity and flow over a backward-facing step. The effects of relaxation factor, number of grid nodes and number of sweeps through the pressure equations are studied to evaluate the performance of the PISO and SIMPLER schemes. Results show that these improved schemes accelerate the convergence rate of the solution generally by a factor of two as compared to the SIMPLE method.
Document ID
19850002641
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Neely, G. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Claus, R. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:86863
E-2327
NASA-TM-86863
Report Number: NAS 1.15:86863
Report Number: E-2327
Report Number: NASA-TM-86863
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: Reno, NV
Country: United States
Start Date: January 14, 1985
End Date: January 17, 1985
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
85N10949
Funding Number(s)
PROJECT: RTOP 505-31-42
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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