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...

Full description

Saved in:
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
Tags: Add Tag
No Tags, Be the first to tag this record!

Internet

https://hdl.handle.net/2134/8902

Similar Items