Experiments in turbulent boundary layers with foreign gas injection

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dc.contributor.author D. I. A. Dunbar en_US
dc.contributor.author L. C. Squire en_US
dc.date.accessioned 2014-10-21T15:50:42Z
dc.date.available 2014-10-21T15:50:42Z
dc.date.issued 1971 en_US
dc.identifier.other ARC/R&M-3696 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/2971
dc.description.abstract An investigation has been made of the properties of turbulent boundary layers in negligible pressure gradient with homogeneous injection of carbon dioxide through a porous surface. Experiments were carried out at Mach numbers of 0.55, 1.8, 2.5 and 3.5 at various blowing rates, the highest rate at M= 3.5 giving symptoms of incipient 'blow-off'. Velocity, temperature and concentration profiles were measured at various stations along the layer and these results have been used to determine skin-friction and shearstress profiles in the boundary layer. This report contains the full results in tabular form and also presents a preliminary analysis of the results. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Experiments in turbulent boundary layers with foreign gas injection en_US

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