Methods of solving the flutter equations in use at R.A.E

dc.contributor.author	T. Niblett	en_US
dc.date.accessioned	2014-10-20T11:05:29Z
dc.date.available	2014-10-20T11:05:29Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-1046	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1059
dc.description.abstract	Details are given of some of the methods of solving the flutter equations which have been programmed in Mercury Autocode at the R.A.E. Included is a method of following the variation of critical speed with a linear variation of the structural inertia, damping or stiffness.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Methods of solving the flutter equations in use at R.A.E	en_US