An experimental investigation of the boundary layer on a porous circular cylinder

Show simple item record

dc.contributor.author D. G. Hurley en_US
dc.contributor.author B. Thwaites en_US
dc.date.accessioned 2014-10-21T15:53:05Z
dc.date.available 2014-10-21T15:53:05Z
dc.date.issued 1951 en_US
dc.identifier.other ARC/R&M-2829 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3384
dc.description.abstract The report describes an experimental investigation of the boundary laver on the surface of a porous circular cylinder at which there is a normal inward velocity. The primary object of the experiments was to test the approximate theory of Ref. 1 for calculating the development of a laminar boundary layer under conditions of continuous suction. The formula given in that reference for calculating the momentum thickness of the layer gave results in accord with the experimental determinations. Owing to practical difficulties in the exploration of the very thin boundary layers and in the determination of the velocity gradient around the surface, other comparisons with the theory (such as the progressive development of the boundary-layer velocity distribution and of the prediction of the separation point) were difficult. Nevertheless reasonable agreement between the theoretical and experimental velocity distributions was obtained particularly for the lower wind speed of the experiment, but no adequate test of the prediction of the separation point was found possible. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title An experimental investigation of the boundary layer on a porous circular cylinder en_US


Files in this item

This item appears in the following Collection(s)

Show simple item record

Search AERADE


Browse

My Account