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Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structuresThe effects of placing a parallel-plate turbulence manipulator in a boundary layer are documented through flow visualization and hot wire measurements. The boundary layer manipulator was designed to manage the large scale structures of turbulence leading to a reduction in surface drag. The differences in the turbulent structure of the boundary layer are summarized to demonstrate differences in various flow properties. The manipulator inhibited the intermittent large scale structure of the turbulent boundary layer for at least 70 boundary layer thicknesses downstream. With the removal of the large scale, the streamwise turbulence intensity levels near the wall were reduced. The downstream distribution of the skin friction was also altered by the introduction of the manipulator.
Document ID
19810021850
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Corke, T. C.
(Illinois Inst. of Tech. Chicago, IL, United States)
Guezennec, Y.
(Illinois Inst. of Tech. Chicago, IL, United States)
Nagib, H. M.
(Illinois Inst. of Tech. Chicago, IL, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1981
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-3444
Accession Number
81N30392
Funding Number(s)
CONTRACT_GRANT: NSG-1591
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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