Modelling infinite length panels using the finite element method

This paper compares three finite element models for determining the buckling and post-buckling performance of infinite length thin walled composite and metal stiffened panels — such as for modeling theoretical aircraft upper wing skin panels — namely single bay, double half-bay and quad half-bay mod...

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Bibliographic Details
Main Authors: Patrick Fenner, Andrew Watson, C.A. Featherston
Format: Default Article
Published: 2016
Subjects:
Mechanical engineering not elsewhere classified
Other engineering not elsewhere classified
Panel buckling
Postbuckling
Finite element method
FEM
Infinite length
Finite strip
FSM
Mechanical Engineering
Engineering not elsewhere classified
Online Access:https://hdl.handle.net/2134/21826
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