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Curvature effects and turbulent boundary layersResults are examined from an experiment conducted to determine quantitatively the secondary factors which affect the response of a turbulent boundary layer to convex curvature and to examine the recovery process after curvature ended. The variation of Stanton number with streamwise distance and with enthalpy thickness Reynolds number for the baseline case is shown. The effect of delta sub .99/R on the velocity of the potential core would have if we extended to the wall with no viscous effects, of free stream acceleration, of an unheated starting length, and of boundary layer maturity are discussed. Mixing length and turbulent Prandtl number models are reviewed.
Document ID
19830010463
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Moffat, R. J.
(Stanford Univ. CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Publication Information
Publication: Von Karman Inst. for Fluid Dyn. Film Cooling and Turbine Blade Heat Transfer, Vol. 1
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
83N18734
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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