The dynamic stability derivatives of a slender wing, a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4

dc.contributor.author	K. J. Turner	en_US
dc.contributor.author	A. Jean Ross	en_US
dc.contributor.author	Geraldine Earley	en_US
dc.date.accessioned	2014-10-20T11:05:02Z
dc.date.available	2014-10-20T11:05:02Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-995	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1008
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The dynamic stability derivatives of a slender wing, a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4	en_US