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Reduced Navier Stokes Relaxation Procedures for Internal FlowsIn spite of significant advancement in the field of high speed computing, flow calculations involving complex geometries and/or flow behavior still require large amounts of CPU time and memory. In order to predict such flows without sacrificing grid convergence and accuracy, adaptive gridding techniques that provide optimal resolution are highly desirable. The present work combines multigrid techniques and domain decomposition concepts to provide local, solution adaptive, grid refinement. Several viscous compressible and incompressible, two and three-dimensional, flows with strong inviscid interaction and/or axial flow reversal, are considered with a segmented multigrid domain decomposition (SMGDD) procedure for which uniform meshes result in each domain. A pressure-based form of flux-vector splitting is applied to the Navier-Stokes equations, which are represented by an implicit lowest-order reduced Navier-Stokes (RNS) system and a purely diffusive, higher-order, deferred-corrector. A trapezoidal or box-like form of discretization insures that all mass conservation properties are satisfied at interfacial and outflow boundaries, even for this primitive-variable non-staggered grid computation. The SMGDD technique presented herein has previously been applied for incompressible two dimensional flows. The present work offers improvement in the gridding strategy, by allowing for disjoint subdomains that provide optimal resolution of disparate flow features. It also extends the SMGDD technique to three dimensional compressible flows. Laminar and turbulent flow in a backward facing step channel is considered; although the procedure is applicable to more severe geometries. The standard K-epsilon model is applied for turbulence closure. For Re greater than 400, differences between two-dimensional theory and experiment are resolved through a three dimensional simulation, which confirms the experimentally observed three dimensionality of the recirculation patterns on the upper and lower surfaces.
Document ID
19970017368
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rubin, Stanley G.
(Cincinnati Univ. OH United States)
Date Acquired
August 17, 2013
Publication Date
May 16, 1997
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:204407
NASA-CR-204407
Report Number: NAS 1.26:204407
Report Number: NASA-CR-204407
Accession Number
97N19658
Funding Number(s)
CONTRACT_GRANT: NAG3-1178
CONTRACT_GRANT: NAG3-397
Distribution Limits
Public
Copyright
Public Use Permitted.
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