Some possible effects of transonic speeds on wing-aileron flutter

dc.contributor.author	E. G. Broadbent	en_US
dc.contributor.author	E. Violet Hartley	en_US
dc.date.accessioned	2014-10-21T15:55:35Z
dc.date.available	2014-10-21T15:55:35Z
dc.date.issued	1959	en_US
dc.identifier.other	ARC/R&M-3258	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3833
dc.description.abstract	A typical wing-aileron combination is taken and ternary flutter calculations between wing bending, wing torsion and aileron rotation are described. The results are plotted as graphs of flutter speed against aileron frequency and the effects of changes in aerodynamic derivatives such as might occur at transonic speeds are investigated. The derivative changes are (1) reduction first in (-hβ) and then in all β derivatives and (2) aft shift of wing aerodynamic centre and aileron aerodynamic centre, separately and together.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Some possible effects of transonic speeds on wing-aileron flutter	en_US