On the flexure of thin built-up wings

dc.contributor.author	G. G. Pope	en_US
dc.date.accessioned	2014-10-21T15:55:43Z
dc.date.available	2014-10-21T15:55:43Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/R&M-3283	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3860
dc.description.abstract	When thin built-up wings experience pure flexure, the surfaces deflect towards the neutral axis of the cross-section due to the 'Brazier' effect. The resulting cross-sectional deformation of symmetrical wings with flat faces between adjacent spars is here analysed, together with the corresponding loss in flexural stiffness.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	On the flexure of thin built-up wings	en_US