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