Pages that link to "Item:Q6560656"
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The following pages link to Post-buckling optimization of composite structures using Koiter's method (Q6560656):
Displaying 6 items.
- A novel reduced-order modeling method for nonlinear buckling analysis and optimization of geometrically imperfect cylinders (Q6553307) (← links)
- A corotational mixed flat shell finite element for the efficient geometrically nonlinear analysis of laminated composite structures (Q6554085) (← links)
- Accurate and efficient \textit{a posteriori} account of geometrical imperfections in Koiter finite element analysis (Q6557572) (← links)
- A reduced-order method for geometrically nonlinear analysis of the wing-upper-skin panels in the presence of buckling (Q6590228) (← links)
- Prediction of geometrically nonlinear behavior for the strength optimization of composite laminates using attention-based Seq2Seq model (Q6641937) (← links)
- Uniform multiple laminates interpolation model and design method for double-double laminates based on multi-material topology optimization (Q6663305) (← links)
