On the axial compression of long, slightly curved panels

dc.contributor.author	G. G. Pope	en_US
dc.date.accessioned	2014-10-21T15:56:18Z
dc.date.available	2014-10-21T15:56:18Z
dc.date.issued	1963	en_US
dc.identifier.other	ARC/R&M-3392	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3974
dc.description.abstract	A finite-deflection analysis is given of the buckling of long, slightly curved panels in compression parallel to the generators, with sides either clamped or simply-supported, and with various combinations of boundary conditions in the middle surface.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	On the axial compression of long, slightly curved panels	en_US