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A New View on Origin, Role and Manipulation of Large Scales in Turbulent Boundary LayersThe potential of passive 'manipulators' for altering the large scale turbulent structures in boundary layers was investigated. Utilizing smoke wire visualization and multisensor probes, the experiment verified that the outer scales could be suppressed by simple arrangements of parallel plates. As a result of suppressing the outer scales in turbulent layers, a decrease in the streamwise growth of the boundary layer thickness was achieved and was coupled with a 30 percent decrease in the local wall friction coefficient. After accounting for the drag on the manipulator plates, the net drag reduction reached a value of 20 percent within 55 boundary layer thicknesses downstream of the device. No evidence for the reoccurrence of the outer scales was present at this streamwise distance thereby suggesting that further reductions in the net drag are attainable. The frequency of occurrence of the wall events is simultaneously dependent on the two parameters, Re2 delta sub 2 and Re sub x. As a result of being able to independently control the inner and outer boundary layer characteristics with these manipulators, a different view of these layers emerged.
Document ID
19830007317
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Corke, T. C.
(Illinois Inst. of Tech. Chicago, IL, United States)
Nagib, H. M.
(Illinois Inst. of Tech. Chicago, IL, United States)
Guezennec, Y. G.
(Illinois Inst. of Tech. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1982
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-165861
NAS 1.26:165861
Report Number: NASA-CR-165861
Report Number: NAS 1.26:165861
Accession Number
83N15588
Funding Number(s)
CONTRACT_GRANT: NSG-1591
PROJECT: RTOP 505-31-23-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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