The dynamic stability derivatives of a slender wing at zero and moderate lift a comparison of theory with free-flight model tests, M 0.8 to 2.0

dc.contributor.author	A. Jean Ross	en_US
dc.contributor.author	Geraldine F. Edwards	en_US
dc.contributor.author	A. P. Waterfall	en_US
dc.date.accessioned	2014-10-20T11:06:41Z
dc.date.available	2014-10-20T11:06:41Z
dc.date.issued	1975	en_US
dc.identifier.other	ARC/CP-1310	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1323
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	The dynamic stability derivatives of a slender wing at zero and moderate lift a comparison of theory with free-flight model tests, M 0.8 to 2.0	en_US