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

dc.contributor.authorCraven, A. H.
dc.date.accessioned2014-09-25T16:04:28Z
dc.date.available2014-09-25T16:04:28Z
dc.date.issued1960-03
dc.description.abstractThis 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.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/8708
dc.language.isoenen_UK
dc.relation.ispartofseriesCollege of Aeronauticsen_UK
dc.relation.ispartofseries129en_UK
dc.relation.ispartofseriesCOA/129en_UK
dc.titleBase pressure at subsonic speeds in the presence of a supersonic jeten_UK
dc.typeReporten_UK

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