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An experimental investigation of turbulent boundary layers along curved surfacesA curved wall tunnel was designed, and an equilibrium turbulent boundary layer was set up on the straight section preceding the curved test section. Turbulent boundary layer flows with uniform and adverse pressure distributions along convex and concave walls were investigated. Hot-wire measurements along the convex surface indicated that turbulent mixing between fluid layers was very much reduced. However, the law of the wall held and the skin friction, thus determined, correlated well with other measurements. Hot-wire measurements along the concave test wall revealed a system of longitudinal vortices inside the boundary layer and confirmed that concave curvature enhances mixing. A self-consistent set of turbulent boundary layer equations for flows along curved surfaces was derived together with a modified eddy viscosity. Solution of these equations together with the modified eddy viscosity gave results that correlated well with the present data on flows along the convex surface with arbitrary pressure distribution. However, it could only be used to predict the mean characteristics of the flow along concave walls because of the existence of the system of longitudinal vortices inside the boundary layer.
Document ID
19720014689
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
So, R. M. C.
(Princeton Univ. NJ, United States)
Mellor, G. L.
(Princeton Univ. NJ, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1972
Publication Information
Publisher: NASA
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-1940
ASM-979
Report Number: NASA-CR-1940
Report Number: ASM-979
Accession Number
72N22339
Funding Number(s)
CONTRACT_GRANT: NGR-31-001-074
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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