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Three-dimensional simulation of vortex breakdownThe integral form of the complete, unsteady, compressible, three-dimensional Navier-Stokes equations in the conservation form, cast in generalized coordinate system, are solved, numerically, to simulate the vortex breakdown phenomenon. The inviscid fluxes are discretized using Roe's upwind-biased flux-difference splitting scheme and the viscous fluxes are discretized using central differencing. Time integration is performed using a backward Euler ADI (alternating direction implicit) scheme. A full approximation multigrid is used to accelerate the convergence to steady state.
Document ID
19900012428
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kuruvila, G.
(NASA Langley Research Center Hampton, VA, United States)
Salas, M. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:102664
NASA-TM-102664
Accession Number
90N21744
Funding Number(s)
PROJECT: RTOP 505-60-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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