Measurements of dynamic stability from three simplified free-flight models of a supersonic research aircraft (Bristol T.188) over the mach number range 1.2 - 2.6

dc.contributor.author	K. J. Turner	en_US
dc.date.accessioned	2014-10-20T11:04:19Z
dc.date.available	2014-10-20T11:04:19Z
dc.date.issued	1965	en_US
dc.identifier.other	ARC/CP-816	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/829
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Measurements of dynamic stability from three simplified free-flight models of a supersonic research aircraft (Bristol T.188) over the mach number range 1.2 - 2.6	en_US