Flight measurements of the dutch roll characteristics of a 60 degree delta wing aircraft (fairey delta 2) at mach numbers from 0.4 to 1.5 with stability derivatives extracted by vector analysis

dc.contributor.author	R. Rose	en_US
dc.date.accessioned	2014-10-20T11:03:20Z
dc.date.available	2014-10-20T11:03:20Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/CP-653	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/666
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Flight measurements of the dutch roll characteristics of a 60 degree delta wing aircraft (fairey delta 2) at mach numbers from 0.4 to 1.5 with stability derivatives extracted by vector analysis	en_US