| dc.creator | Harris, T. M. | |
| dc.date | 2017-06-23T08:52:42Z | |
| dc.date | 2017-06-23T08:52:42Z | |
| dc.date | 1962-10 | |
| dc.date.accessioned | 2022-05-09T10:07:11Z | |
| dc.date.available | 2022-05-09T10:07:11Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/12104 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4496 | |
| dc.description | Wind tunnel tests have been made on a circular-wing with 90° downward peripheral blowing both in and out of ground effect. Tests made with two slot widths, a range of blowing pressures and choked jets, indicate that Cu is a unifying parameter for this type of test. The windspeed was varied between 0 to 200 ft/sec. at zero incidence and the static pressure distribution on both top and bottom surfaces was measured. The sum of the integrated pressures on both upper and lower surfaces 3 agreed reasonably well with the measured overall lift. Flow visualisation on a streamwise plate beneath the model showed the vortex system and the eventual 4 collapse of the forward jet with increasing windspeed. | |
| dc.language | en | |
| dc.publisher | College of Aeronautics | |
| dc.relation | CoA/N-133 | |
| dc.relation | 133 | |
| dc.title | Some tests on a circular ground effect machine with forward speed | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_N_133_1962.pdf | 3.546Mb | application/pdf |
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