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Confined turbulent swirling recirculating flow predictionsThe capability and the accuracy of the STARPIC computer code in predicting confined turbulent swirling recirculating flows is presented. Inlet flow boundary conditions were demonstrated to be extremely important in simulating a flowfield via numerical calculations. The degree of swirl strength and expansion ratio have strong effects on the characteristics of swirling flow. In a nonswirling flow, a large corner recirculation zone exists in the flowfield with an expansion ratio greater than one. However, as the degree of inlet swirl increases, the size of this zone decreases and a central recirculation zone appears near the inlet. Generally, the size of the central zone increased with swirl strength and expansion ratio. Neither the standard k-epsilon turbulence mode nor its previous extensions show effective capability for predicting confined turbulent swirling recirculating flows. However, either reduced optimum values of three parameters in the mode or the empirical C sub mu formulation obtained via careful analysis of available turbulence measurements, can provide more acceptable accuracy in the prediction of these swirling flows.
Document ID
19850018405
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Abujelala, M. T.
(Oklahoma State Univ. Stillwater, OK, United States)
Lilley, D. G.
(Oklahoma State Univ. Stillwater, OK, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:174917
NASA-CR-174917
Report Number: NAS 1.26:174917
Report Number: NASA-CR-174917
Accession Number
85N26716
Funding Number(s)
CONTRACT_GRANT: NAG3-74
PROJECT: RTOP 533-04-1A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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