On the stressing of multi-rib thin wings of low aspect ratio and rectangular plan-form

dc.contributor.author	L. S. D. Morley	en_US
dc.date.accessioned	2014-10-21T15:54:19Z
dc.date.available	2014-10-21T15:54:19Z
dc.date.issued	1955	en_US
dc.identifier.other	ARC/R&M-3052	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3622
dc.description.abstract	Exact theories are used to examine tile validity of certain methods of wing stressing when they are applied to thin wings of low aspect ratio. Attention is confined to thetwo spar multi-rib wing having rectangular cross-section and rectangular plan-form.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	On the stressing of multi-rib thin wings of low aspect ratio and rectangular plan-form	en_US