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Spur-type instability observed on numerically simulated vortex filamentsAn instability observed on vortex filaments during numerical simulations of the three-dimensional, time-dependent dynamics of vortex wakes is studied to determine when and why it occurs. It is concluded that the observed instability is a consequence of the use of straight-line vortex segments of finite length to model continuously curving vortex filaments. The instability appears to occur only when the link length is a sizable fraction of the vortex span and, therefore, is not expected in an experiment. Guidelines are then given that help avoid numerical instabilities when vortex filaments are used in flow simulations.
Document ID
19890028724
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rossow, Vernon J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
September 1, 1988
Publication Information
Publication: Journal of Aircraft
Volume: 25
ISSN: 0021-8669
Subject Category
Aerodynamics
Accession Number
89A16095
Distribution Limits
Public
Copyright
Other

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