| dc.creator | Craven, A. H. | |
| dc.date | 2014-09-25T16:04:28Z | |
| dc.date | 2014-09-25T16:04:28Z | |
| dc.date | 1960-03 | |
| dc.date.accessioned | 2022-05-09T10:17:26Z | |
| dc.date.available | 2022-05-09T10:17:26Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/8708 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4803 | |
| dc.description | 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. | |
| dc.language | en | |
| dc.relation | College of Aeronautics | |
| dc.relation | 129 | |
| dc.relation | COA/129 | |
| dc.title | Base pressure at subsonic speeds in the presence of a supersonic jet | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_Report_No_129_March_1960.pdf | 9.534Mb | application/pdf |
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