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Three-dimensional compressible turbulent computations for a nondiffusing S-ductThe PARC3D code was used to compute the compressible turbulent flow within a three dimensional, nondiffusing S-duct. A frame of reference is provided for future computational fluid dynamics studies of internal flows with strong secondary flows and provides an understanding of the performance characteristics of a typical S-duct with attached flow. The predicted results, obtained with both H- and O-grids, are compared with the experimental wall pressure, static and total pressure fields, and velocity vectors. Additionally, computed boundary layer thickness, velocity profiles in wall coordinates, and skin friction values are presented.
Document ID
19920022996
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harloff, G. J.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Debonis, J. R.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Smith, C. F.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Bruns, J. E.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1992
Publication Information
Publisher: NASA. Lewis Research Center
Subject Category
Aerodynamics
Report/Patent Number
E-6173
NAS 1.26:4391
NASA-CR-4391
Accession Number
92N32240
Funding Number(s)
PROJECT: RTOP 533-02-30
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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