Downwash measurements behind a 12-ft diameter helicopter rotor in the 24-ft wind tunnel

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