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Characterization of flow in a scroll ductA quantitative, flow visualization study was made of a partially elliptic cross section, inward curving duct (scroll duct), with an axial outflow through a vaneless annular cutlet. The working fluid was water, with a Re(d) of 40,000 at the inlet to the scroll duct, this Reynolds number being representative of the conditions in an actual gas turbine scroll. Both still and high speed moving pictures of fluorescein dye injected into the flow and illuminated by an argon ion laser were used to document the flow. Strong secondary flow, similar to the secondary flow in a pipe bend, was found in the bottom half of the scroll within the first 180 degs of turning. The pressure field set up by the turning duct was strong enough to affect the inlet flow condition. At 90 degs downstream, the large scale secondary flow was found to be oscillatory in nature. The exit flow was nonuniform in the annular exit. By 270 degs downstream, the flow appeared unorganized with no distinctive secondary flow pattern. Large scale structures from the upstream core region appeared by 90 degs and continued through the duct to reenter at the inlet section.
Document ID
19910016053
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Begg, E. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Bennett, J. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:188612
NASA-CR-188612
Report Number: NAS 1.26:188612
Report Number: NASA-CR-188612
Accession Number
91N25367
Funding Number(s)
CONTRACT_GRANT: NAG3-484
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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