Independence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speed

dc.contributor.author	Bryce, W. W.
dc.date.accessioned	2013-07-19T11:36:10Z
dc.date.available	2013-07-19T11:36:10Z
dc.date.issued	1956-11
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7988
dc.description.abstract	A radial parabolic induced velocity distribution agreeing closely with flight measurements has been used for the hovering case. Continues...	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics, Cranfield	en_UK
dc.relation.ispartofseries	College Report	en_UK
dc.relation.ispartofseries	110	en_UK
dc.title	Independence of helicopter rotor derivatives under non-uniformity of induced velocity distribution at low forward speed	en_UK
dc.type	Report	en_UK