The present work deals with a generalization of geometrically linear shear deformation theory for multilayered anisotropic shells of general shape.
A numerical method apt to analyse compact cross-sections of general shape under bending, compression and given non-linear strain distributions of general shape is presented.
In this paper, we consider sensing regions of general shape, because this reflects a more realistic scenario.
The overall numerical algorithm handles boundaries of general shape using regular structured grids with no deterioration of accuracy.
The expressions apply to a body of general shape that carries no net native charge; illustrative examples are provided for ellipsoidal and spheroidal bodies.
The structural tree method (STM) was developed to compute the assembly dimension variation from the deformations of individual components, as well as the deformation of general shape composite components.
Numerical simulations confirm the predictions of the stability analysis even for complex problems, and show that the AMP algorithm remains stable, without sub-iterations, for light and even zero-mass three-dimensional rigid bodies of general shape.
A few numerical examples are shown Theassess the aprocedureisy of the method, itsimpleutotimplementort and some convergence issues.
