| dc.creator | Craven, A. H. | |
| dc.date | 2017-02-24T12:14:51Z | |
| dc.date | 2017-02-24T12:14:51Z | |
| dc.date | 1957-04 | |
| dc.date.accessioned | 2022-05-09T09:47:01Z | |
| dc.date.available | 2022-05-09T09:47:01Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/11493 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4172 | |
| dc.description | This report contains the results of an experimental investigation into the interference of a ,rearward facing undeflected jet on the flow over three afterbody shapes at subsonic speeds. The tests were performed at a Reynolds number of 0.3 x 10(6) based on body diameter. It was found that the form (or pressure) drag coefficient of the bluff afterbody of a right cylinder increased appreciably with increase in jet thrust coefficient. A similar but much smaller increase in form drag was found on an ellipsoidal afterbody and a 'boat-tail'. The effect of the jet was found to extend to approximately three body diameters upstream of the jet exit but that beyond one body diameter the effect was very small. | |
| dc.language | en | |
| dc.publisher | College of Aeronautics | |
| dc.relation | CoA/N-60 | |
| dc.relation | 60 | |
| dc.title | The interference of a rearward facing jet on the flow over three representative afterbody shapes in a uniform subsonic flow | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_N_60_1957.pdf | 2.200Mb | application/pdf |
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