Streamwise edge effects in the turbulent boundary layer on a flat plate of finite aspect ratio

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dc.contributor.author E. B. Davies en_US
dc.contributor.author A. D. Young en_US
dc.date.accessioned 2014-10-21T15:56:11Z
dc.date.available 2014-10-21T15:56:11Z
dc.date.issued 1963 en_US
dc.identifier.other ARC/R&M-3367 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3950
dc.description.abstract A detailed investigation of the turbulent boundary layer on a flat plate of finite aspect ratio at zero incidence has been made, incorporating measurements of mean velocity profiles and skin friction over one surface of the plate. Skin friction was measured using Prof. Preston's surface-tube technique with the N.P.L. calibration, and this is justified by comparison with the measured momentum defect. These results are compared with others recorded on a 'two-dimensional' plate (i.e. one that spanned the wind tunnel), and the effects of the streamwise edges on the boundary-layer flow on the plate surface are shown to be limited to regions of the plate surface near the edges of the order of a boundary-layer thickness in width. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Streamwise edge effects in the turbulent boundary layer on a flat plate of finite aspect ratio en_US


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