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Measurements of laminar and turbulent flow in a curved duct with thin inlet boundary layersLaser Doppler velocimetry was used to measure the laminar and turbulent flow in a 90 deg square bend of strong curvature. The boundary layers at the inlet to the bend were approximately 25 percent and 15 percent of the hydraulic diameter for the laminar and turbulent flows, respectively. The development of the pressure driven secondary motion is more rapid for laminar flow: the maximum cross stream component measured was 60 percent of the bulk velocity in contrast to 40 percent for turbulent flow. The streamwise isotachs show that, for laminar flow, large velocities are found progressively nearer to the outer radius of the bend and along the sidewalls. For turbulent flow, the isotachs move towards the inner radius until about 60 deg around the bend where strong secondary motion results in a similar redistribution. Turbulence level and shear stress measurements are also presented.
Document ID
19810007898
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Taylor, A. M. K. P.
(Imperial Coll. of Science and Technology London, United Kingdom)
Whitelaw, J. H.
(Imperial Coll. of Science and Technology London, United Kingdom)
Yianneskis, M.
(Imperial Coll. of Science and Technology London, United Kingdom)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
FS-80-29
NASA-CR-3367
Accession Number
81N16414
Funding Number(s)
CONTRACT_GRANT: NASW-3258
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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