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<journal-meta>
<journal-id>International Journal of Aerospace and Lightweight Structures</journal-id>
<publication_date>2012</publication_date>
<volume>2</volume>
<issue>2</issue>
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<doi>10.3850/S2010428612000323</doi>
<article-title>The Ultimate Strength of Stiffened Panel with Beam-Column Buckling</article-title>
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<author>Bao Zhanga<sup>a</sup> and Qun Sun</author>
<author-citation>Zhanga, Bao; Sun, Qun</author-citation>

<aff>School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China.</aff>
<email><a href="mailto:bzhang.nwpu@gmail.com"><sup>a</sup>bzhang.nwpu@gmail.com</a></email>

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<abstract>
<title>ABSTRACT</title>
<p>The ultimate strength of a stiffened panel with beam-column buckling is investigated
using the beam-column approaches. The ultimate strength of the beam-column is
obtained by the analytical formulas (the Johnson-Ostenfeld Formula and the Perry-
Robertson Formula) and finite element method, which incorporates the effective width
formulas (Von Karman and the Winter formulas) here. Meanwhile, a novel numerical
method is developed to calculate the effective width of the beam-column. Furthermore,
the ultimate strength of the whole stiffened panel is deduced using that of the single
beam-column. Comparisons between these proposed methods and the nonlinear finite
element analysis (the CAE software is ABAQUS) are performed. The results show that
good accuracy can be achieved using the proposed methods, especially for the beamcolumn
approach based on the finite element analysis. It suggests that the methods can
predict the ultimate strength of a whole stiffened panel accurately and effectively.</p><p><italic>Keywords: Beam-column, Effective width, Nonlinear FEM.</italic></p>
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