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The effect of opposing unsteady vorticity on turbulent wall flowA cylinder and a thin plate were placed close together in a flow adjacent to a wall to study the effects on the turbulent boundary layer. Different spacings of the cylinder and plate within the shear flow were investigated to assess the possibility of lowering the production of fluctuating vorticity in the boundary layer by generating a fluctuating vorticity of opposite sign. Streakline photographs visualized changes in the flow induced by alterations in the cylinder/plate separation distance, the flow velocity and the angle of attack of the thin plate. Drag data were also acquired with varying thicknesses of the thin plate and diameters of the cylinder. Downstream skin friction reductions were obtained with the production of unsteady control vortices with a low turbulence boundary layer. Up to 4 percent drag reduction was also observed when the cylinder was sufficiently far from the wall.
Document ID
19850043792
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goodman, W. L.
(NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-0550
Accession Number
85A25943
Distribution Limits
Public
Copyright
Other

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