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Numerical simulation of vortex breakdown by the vortex-filament methodThe vortex filament method was applied to the simulation of vortex breakdown. The principal vortex region was represented by multiple filaments, and an axial velocity component was induced by a spiral winding of the filaments. First, an accuracy check was performed for a cylindrical swirling flow with simple analytical expressions for the axial and theta velocities. The result suggests that the flow field is simulated to any accuracy by increasing the number of filaments. Second, an axisymmetric type vortex breakdown was simulated, with experimental data serving as upstream conditions. The calculated axial and theta velocity contours show the breakdown of the vortex, including a rapid change in the vortex core, followed axially by a recovery zone and then a second breakdown. When three dimensional initial data are used the second breakdown appears to be of the spiral type in correspondence with experimental observations. The present method is easily used to simulate other types of vortex breakdown or other vortex flows with axial velocity.
Document ID
19830021365
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nakamura, Y.
(NASA Ames Research Center Moffett Field, CA, United States)
Leonard, A.
(NASA Ames Research Center Moffett Field, CA, United States)
Spalart, P. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
A-9263
NAS 1.15:84334
NASA-TM-84334
Report Number: A-9263
Report Number: NAS 1.15:84334
Report Number: NASA-TM-84334
Accession Number
83N29636
Funding Number(s)
PROJECT: RTOP 505-31-21-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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