The calculation of the rotary lateral stability derivatives of a jet-flapped wing

dc.contributor.author	H. H. B. M. Thomas	en_US
dc.contributor.author	A. J. Ross	en_US
dc.date.accessioned	2014-10-21T15:55:41Z
dc.date.available	2014-10-21T15:55:41Z
dc.date.issued	1958	en_US
dc.identifier.other	ARC/R&M-3277	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3853
dc.description.abstract	The problem of calculating the rotary lateral stability derivatives for a straight wing with a thin jet emerging at the trailing edge is considered. Based on Maskell and Spence's analysis of the effect of finite aspect ratio on lift and drag a solution is described which shows that the presence of the jet has considerable effect on the stability derivatives.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The calculation of the rotary lateral stability derivatives of a jet-flapped wing	en_US