| T-stiffened flat laminated composite panel under combined in-plane loads Nx and Nxy and normal pressure |
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| Objective versus design iterations during 8 successive executions of the PANDA2 processor, PANDAOPT |
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| Plan view of a STAGS model of the T-stiffened flat panel under combined in-plane loading, Nx and Nxy and normal pressure, p |
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| Linear bifurcation buckling mode of the optimized T-stiffened panel from STAGS |
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| STAGS prediction of the normal deflection of the laminated composite T-stiffened panel at four load steps |
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| Results from two successive STAGS nonlinear static equilibrium runs |
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| STAGS predictions of the postbuckling deformation of the T-stiffened laminated composite panel |
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| STAGS prediction of contours of normal displacement in the far-postbuckling regime |
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| Various types of stress margins computed by PANDA2 |
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