The effect of steady tailplane lift on the oscillatory behaviour of a T-tail flutter model at high subsonic speeds

dc.contributor.author	R. Gray	en_US
dc.contributor.author	D. A. Drane	en_US
dc.date.accessioned	2014-10-21T15:50:54Z
dc.date.available	2014-10-21T15:50:54Z
dc.date.issued	1972	en_US
dc.identifier.other	ARC/R&M-3745	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3024
dc.description.abstract	The oscillatory behaviour of a T-tail has been investigated at high subsonic Mach numbers on an aeroelastic model having tailplane settings of zero and three degrees. There is broadly satisfactory agreement between calculated and measured values of modal frequency and damping. The comparison has been based mainly on the flutter margin criterion of Zimmerman and Weissenburger, since the more conventional comparisons are inconclusive.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The effect of steady tailplane lift on the oscillatory behaviour of a T-tail flutter model at high subsonic speeds	en_US