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Navier-Stokes analysis of three-dimensional S-ductsFull 3D Navier-Stokes computational results are presented for compressible flows within nondiffusing and diffusing S-ducts. The present study provides an understanding of the performance characteristics of typical S-ducts with attached and separated flows and provides a frame of reference for future computational fluid dynamic studies of internal flows with strong secondary flows. The predicted results, which were obtained using both H- and O-grids, are compared with the experimental wall pressures, static and total pressure fields, and velocity vectors. In addition, computed boundary-layer thickness, velocity profiles in wall coordinates and skin friction values are presented. The inviscid contributions to the secondary flows are quantified. The S-duct entrance Mach number was 0.6, and the Reynolds number was 1.76 x 10 exp 6 based on the upstream duct diameter.
Document ID
19930061149
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Harloff, G. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Smith, C. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Bruns, J. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Debonis, J. R.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
August 16, 2013
Publication Date
August 1, 1993
Publication Information
Publication: Journal of Aircraft
Volume: 30
Issue: 4
ISSN: 0021-8669
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0021-8669
Accession Number
93A45146
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Other

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