Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4

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dc.contributor.authorEmslie, K.
dc.contributor.authorHosking, L.
dc.contributor.authorMarshall, W. S. D.
dc.date.accessioned2012-09-11T10:28:04Z
dc.date.available2012-09-11T10:28:04Z
dc.date.issued1953-02
dc.description.abstractVisual methods have been used together with a yawmeter to illustrate conditions of flow in the boundary layer over a sweptback wing. It was found out that at moderate incidences a marked outflow in the boundary layer was developed. Continues …en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7559
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reportsen_UK
dc.relation.ispartofseries69en_UK
dc.titleSome experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4en_UK
dc.typeReporten_UK

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