Dynamics of the deformable aeroplane part 1 the equations of motion part 2 a study of the trim state and longitudinal stability of the slender integrated aeroplane configuration

dc.contributor.author	R. D. Milne	en_US
dc.date.accessioned	2014-10-21T15:55:56Z
dc.date.available	2014-10-21T15:55:56Z
dc.date.issued	1962	en_US
dc.identifier.other	ARC/R&M-3345	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3926
dc.description.abstract	An integrated analytical treatment is presented which deals with the equilibrium and stability of the flexible aeroplane in flight. The analysis embodies those methods currently employed to investigate the behaviour of the flexible aeroplane stemming on the one hand from the stability theory of the rigid aeroplane and on the other from conventional aeroelastic studies. The integrated treatment serves to clarify the regions of application of these restricted methods.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Dynamics of the deformable aeroplane part 1 the equations of motion part 2 a study of the trim state and longitudinal stability of the slender integrated aeroplane configuration	en_US