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Confined swirling flow predictionsThe validity of flowfield predictions resulting from the choice of inlet velocity profiles is assessed. Results demonstrate that realistic predictions are forthcoming only from the inclusion of realistic axial, radial and swirl velocity profiles as inlet conditions. Predictions are then exhibited for a range of swirl strengths phi = 0, 38, 45, 60 and 70 degrees using measured inlet axial, radial and swirl velocity profiles in each case. Downstream nozzle effects (two blockage size at two axial locations) are included. The ensuing flowfields are characterized via velocity profiles and streamline patterns, and illustrate the large-scale effects of inlet swirl and outlet nozzles on flowfields.
Document ID
19830035428
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Abujelala, M. T.
(Oklahoma State Univ. Stillwater, OK, United States)
Lilley, D. G.
(Oklahoma State University Stillwater, OK, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 83-0316
Report Number: AIAA PAPER 83-0316
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A16646
Funding Number(s)
CONTRACT_GRANT: NAG3-74
Distribution Limits
Public
Copyright
Other

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