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Experimental Study of a Three-Dimensional Shear-Driven Turbulent Boundary Layer with Streamwise Adverse Pressure GradientThe effects of a strong adverse pressure gradient on a three-dimensional turbulent boundary layer are studied in an axisymmetric spinning cylinder geometry. Velocity measurements made with a three-component laser Doppler velocimeter include all three mean flow components, all six Reynolds stress components, and all ten triple-product correlations. Reynolds stress diminishes as the flow becomes three-dimensional. Lower levels of shear stress were seen to persist under adverse pressure gradient conditions. This low level of stress was seen to roughly correlate with the magnitude of cross-flow (relative to free stream flow) for this experiment as well as most of the other experiments in the literature. Variations in pressure gradient do not appear to alter this correlation. For this reason, it is hypothesized that a three-dimensional boundary layer is more prone to separate than a two-dimensional boundary layer, although it could not be directly shown here. None of the computations performed with either a Prandtl mixing length, k-epsilon, or a Launder-Reece-Rodi full Reynolds-stress model were able to predict the reduction in Reynolds stress.
Document ID
19930015352
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Driver, David M.
(NASA Ames Research Center Moffett Field, CA, United States)
Johnston, James P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 15, 2013
Publication Date
May 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-102211
NAS 1.15:102211
NONP-NASA-SUPPL-CD-ROM-93-159790
A-89104
Report Number: NASA-TM-102211
Report Number: NAS 1.15:102211
Report Number: NONP-NASA-SUPPL-CD-ROM-93-159790
Report Number: A-89104
Accession Number
93N24541
Funding Number(s)
PROJECT: RTOP 505-60-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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