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The use of tools based on classical form-finding procedures as dynamic relaxation is the main trend today; different mechanical models with 3, 4 or 6 degrees of freedom have been implemented for modelling the bending effect.
The energy finite element analysis (EFEA) is employed for modelling the bending behavior of the beams and the conventional finite element analysis (FEA) is utilized for modelling the longitudinal vibration in the beams.
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The strategy is designed by modeling the bending process.
A beam finite-element model that accounts for braid angle and strap stiffness was developed to model the bending response of the inflatable, braided, strapped beams and arches.
To accurately model the bending stiffness of the composite, an offset of (h + t)/2 is used for the truss elements (see Fig. 2).
Furthermore, it naturally has the capability of modelling the bending-membrane coupling that occurs on free vibration of VSCL plates with unsymmetric stacking sequences.
In this model, the bending deflection of blade and the casing deformation during rubbing are taken into account.
To illustrate the new model, the bending problem of a simply supported bi-layered square micro-plate subjected to constant distributed load is solved.
To illustrate the new model, the bending problem of a bilayered cantilever microbeam subjected to a moment at the free end is solved.
We model the bending experiments of Tytell and Cohen [6] by assuming that bending activates the edge cells of only one segment.
The problem ((P^{f,g}_{lambda,mu})) models the bending equilibrium of simply supported extensible beams on nonlinear foundations.
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