Buckling load reduction for stiffened panels due to cutouts in ribs

In aerospace structures it is common to find stiffened panels with transverse supporting structures, e.g. wing ribs or fuselage frames. Incorporating cutouts into these supporting structures to allow the stringers to pass through freely considerably reduces the buckling load of the panels. It is sho...

Full description

Bibliographic Details

Main Authors:	Andrew Watson, F.W. Williams, David Kennedy
Format:	Default Article
Published:	1998
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/2134/8694
Tags:	Add Tag No Tags, Be the first to tag this record!