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Modeling Vortex Generators in a Navier-Stokes CodeA source-term model that simulates the effects of vortex generators was implemented into the Wind-US Navier-Stokes code. The source term added to the Navier-Stokes equations simulates the lift force that would result from a vane-type vortex generator in the flowfield. The implementation is user-friendly, requiring the user to specify only three quantities for each desired vortex generator: the range of grid points over which the force is to be applied and the planform area and angle of incidence of the physical vane. The model behavior was evaluated for subsonic flow in a rectangular duct with a single vane vortex generator, subsonic flow in an S-duct with 22 corotating vortex generators, and supersonic flow in a rectangular duct with a counter-rotating vortex-generator pair. The model was also used to successfully simulate microramps in supersonic flow by treating each microramp as a pair of vanes with opposite angles of incidence. The validation results indicate that the source-term vortex-generator model provides a useful tool for screening vortex-generator configurations and gives comparable results to solutions computed using gridded vanes.
Document ID
20110016237
Acquisition Source
Glenn Research Center
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Dudek, Julianne C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
April 1, 2011
Publication Information
Publication: AIAA Journal
Volume: 49
Issue: 4
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2010-0032
E-17922
Report Number: AIAA Paper 2010-0032
Report Number: E-17922
Funding Number(s)
WBS: WBS 984754.02.07.03.12.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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