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and non-shell (beam, plate, ring, arch, etc).
The workpieces with geometries of a beam, plate and shell are considered.
First, an applicability validation of the presented method was done by a vibration test using a cantilevered beam plate.
By these formulations, the physically-based nonlocal model can be conveniently expanded into beam, plate and shell.
The technique can be easily incorporated into any finite element analysis programme for which the beam, plate and shell elements etc. satisfy the Reissner Mindlin assumption.
This chapter elucidates the aforementioned class of problems applied to beam, plate, and shell systems by examining the basic non-linear equilibrium equations.
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Also various failure modes occurred for such FRP-plated steel beams; plate end debonding in an FRP-plated steel beam is the basic mode of failure.
The proposed model is verified using laminated composite beam plates.
It is assumed that beam plates are hinged together along their longitudinal edges.
However, the conclusions are applicable for any tension face beam plating.
Requirements for the framework are discussed based on the features of beam-plate structure design process first.
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