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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. 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 can be simulated to any accuracy by increasing the number of filaments. 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 can easily be used to simulate other types of vortex breakdown or other vortex flows with axial velocity.
Document ID
19840004058
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
August 12, 2013
Publication Date
July 1, 1983
Publication Information
Publication: AGARD Aerodyn. of Vortical Type Flows in Three Dimensions
Subject Category
Aerodynamics
Accession Number
84N12126
Distribution Limits
Public
Copyright
Other
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