dc.contributor.author |
R. A. Fail |
en_US |
dc.contributor.author |
R. C. W. Eyre |
en_US |
dc.date.accessioned |
2014-10-21T15:52:59Z |
|
dc.date.available |
2014-10-21T15:52:59Z |
|
dc.date.issued |
1949 |
en_US |
dc.identifier.other |
ARC/R&M-2810 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3363 |
|
dc.description.abstract |
Some measurements of downwash have been made in a plane behind a 12-ft diameter helicopter rotor over a range of shaft inclination and tip speed ratio. In the various operating conditions, the tunnel tests are in reasonable agreement with the theoretical results for the appropriate type of loading. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Downwash measurements behind a 12-ft diameter helicopter rotor in the 24-ft wind tunnel |
en_US |