Base pressure at subsonic speeds in the presence of a supersonic jet

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dc.contributor.author Craven, A. H.
dc.date.accessioned 2014-09-25T16:04:28Z
dc.date.available 2014-09-25T16:04:28Z
dc.date.issued 1960-03
dc.identifier.uri http://dspace.lib.cranfield.ac.uk/handle/1826/8708
dc.description.abstract This paper presents the results of an experimental investigation into the effect of supersonic jets upon the base pressure of a bluff cylinder in a uniform subsonic flow. The ratio of jot diameter to base diameter was 0.1875. Jet stagnation pressures giving slight under-expansion of the jet cause an increase in the base pressure but for larger jet stagnation pressures the base pressure is again reduced. A simple theory, based on a momentum integral, shows the dependence of the base drag upon the jet and free stream speeds and upon the dimensions of the jet and the base. en_UK
dc.language.iso en en_UK
dc.relation.ispartofseries College of Aeronautics en_UK
dc.relation.ispartofseries 129 en_UK
dc.relation.ispartofseries COA/129 en_UK
dc.title Base pressure at subsonic speeds in the presence of a supersonic jet en_UK
dc.type Report en_UK


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