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The influence of free-stream turbulence on separation of turbulent boundary layers in incompressible, two-dimensional flowExperiments were conducted to determine if free-stream turbulence scale affects separation of turbulent boundary layers. In consideration of possible interrelation between scale and intensity of turbulence, the latter characteristic also was varied and its role was evaluated. Flow over a 2-dimensional airfoil in a subsonic wind tunnel was studied with the aid of hot-wire anemometry, liquid-film flow visualization, a Preston tube, and static pressure measurements. Profiles of velocity, relative turbulence intensity, and integral scale in the boundary layer were measured. Detachment boundary was determined for various angles of attack and free-stream turbulence. The free-stream turbulence intensity and scale were found to spread into the entire turbulent boundary layer, but the effect decreased as the airfoil surface was approached. When the changes in stream turbulence were such that the boundary layer velocity profiles were unchanged, detachment location was not significantly affected by the variations of intensity and scale. Pressure distribution remained the key factor in determining detachment location.
Document ID
19870016849
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Potter, J. Leith
(Vanderbilt Univ. Nashville, TN, United States)
Barnett, R. Joel
(Vanderbilt Univ. Nashville, TN, United States)
Fisher, Carl E.
(Vanderbilt Univ. Nashville, TN, United States)
Koukousakis, Costas E.
(Vanderbilt Univ. Nashville, TN, United States)
Date Acquired
September 5, 2013
Publication Date
December 22, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-180638
NAS 1.26:180638
Accession Number
87N26282
Funding Number(s)
CONTRACT_GRANT: NAG1-483
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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