Postbuckling of stiffened panels using strut, strip, and finite element methods

Postbuckling results are presented for isotropic stiffened panels loaded in compression. Comparisons are made between single-bay and double-bay nite element (FE) models (where “bay” denotes a repeating portion, between supports, in the load/length direction) and a new strut model, following a Shanle...

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Bibliographic Details

Main Authors:	M. Lillico, R. Butler, G.W. Hunt, Andrew Watson, David Kennedy
Format:	Default Article
Published:	2003
Subjects:	Aerospace engineering not elsewhere classified Mechanical engineering not elsewhere classified Other engineering not elsewhere classified untagged Aerospace Engineering Mechanical Engineering Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/8902
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