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Application of a computational model for vortex generators in subsonic internal flowsA model for the analysis of vortex generators in a fully viscous subsonic internal flow is evaluated. A vorticity source term is used in a modified form of the Parabolized Navier-Stokes equations to model the shed vortex. Computed results are compared with idealized flow vortex paths, and with experimental data for vortex generators embedded in a thick turbulent boundary layer. The analysis is also compared with experimental data for a separated diffusing S-duct and for a diffusing S-duct with vortex generators. Quantitative comparisons are shown for the latter three cases. Emphasis is placed on verifying the ability of the model to predict global distortions in the flow field.
Document ID
19860017073
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kunik, W. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:87327
E-3072
AIAA PAPER 86-1458
NASA-TM-87327
Meeting Information
Meeting: Joint Propulsion Conference
Location: Huntsville, AL
Country: United States
Start Date: June 16, 1986
End Date: June 18, 1986
Sponsors: ASME, ASEE, SAE, AIAA
Accession Number
86N26545
Funding Number(s)
PROJECT: RTOP 505-62-61
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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