The prevention of binary flutter by artificial damping

dc.contributor.author	R. A. Frazer	en_US
dc.date.accessioned	2014-10-21T15:56:23Z
dc.date.available	2014-10-21T15:56:23Z
dc.date.issued	1944	en_US
dc.identifier.other	ARC/R&M-2552	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3999
dc.description.abstract	Formulae are obtained which provide an estimate of the amount of artificial control needed to prevent binary flutter. Results are expressed in terms of a 'minimum damping multiplier' R, defined as the ratio of the least direct damping coefficient required for absolute flutter prevention to the 'natural' direct aerodynamic damping coefficient of the control surface concerned. Numerical results are obtained for five different types of aircraft.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The prevention of binary flutter by artificial damping	en_US