One of the current problems connected with multilayer composite structures concerns
the analysis of the distribution of the stresses around peculiarities (free edge
and loaded edge) and at the interfaces of each layer. This work presents a
new shear stress function in the form of the exponential function to predict
the mechanical behavior of multilayered laminated composite structures.
As a case study, the mechanical behavior of a laminated composite beam
is
examined. The results are compared with the Touratier model
sine and the
two-dimensional finite element method studied. Results show that this new model is
more precise than older ones when compared with results obtained by finite element
analysis. To introduce continuity on the interfaces of each layer, the new
exponential model is used with Ossadzow kinematics. The equilibrium equations
and natural boundary conditions are derived from the principle of virtual
power.
Keywords
boron fiber, laminate theory, interface, stress transfer,
finite element analysis