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Control-volume based Navier-Stokes equation solver valid at all flow velocitiesA control-volume based finite difference method to solve the Reynolds averaged Navier-Stokes equations is presented. A pressure correction equation valid at all flow velocities and a pressure staggered grid layout are used in the method. Example problems presented herein include: a developing laminar channel flow, developing laminar pipe flow, a lid-driven square cavity flow, a laminar flow through a 90-degree bent channel, a laminar polar cavity flow, and a turbulent supersonic flow over a compression ramp. A k-epsilon turbulence model supplemented with a near-wall turbulence model was used to solve the turbulent flow. It is shown that the method yields accurate computational results even when highly skewed, unequally spaced, curved grids are used. It is also shown that the method is strongly convergent for high Reynolds number flows.
Document ID
19890011036
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kim, S.-W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-101488
NAS 1.15:101488
ICOMP-89-5
E-4629
Report Number: NASA-TM-101488
Report Number: NAS 1.15:101488
Report Number: ICOMP-89-5
Report Number: E-4629
Accession Number
89N20407
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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