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Navier-Stokes analysis and experimental data comparison of compressible flow in a diffusing S-ductFull three-dimensional Navier-Stokes computational results are compared with new experimental measurements for the flowfield within a round diffusing S-duct. The present study extends previous computational and experimental results for a similar smaller scale S-duct. Predicted results are compared with the experimental static and total pressure fields, and velocity vectors. Additionally, wall pressures, velocity profiles in wall coordinates, and skin friction values are presented. The CFD results employ algebraic and k-epsilon turbulence models. The CFD computed and experimentally determined separated flowfield is carefully examined.
Document ID
19920024502
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harloff, Gary J.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Reichert, Bruce A.
(NASA Lewis Research Center Cleveland, OH, United States)
Wellborn, Steven R.
(Iowa State Univ. of Science and Technology Ames., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-7062
AIAA PAPER 92-2699
NAS 1.15:105683
NASA-TM-105683
Meeting Information
Meeting: Applied Aerodynamics Conference Exhibit
Location: Palo Alto, CA
Country: United States
Start Date: June 22, 1992
End Date: June 24, 1992
Sponsors: AIAA
Accession Number
92N33746
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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