The paper deals with the formulation of the nonlinear equations govern
ing the mechanical behavior of anisotropic, laminated Timoshenko beams
having any number of arbitrarily positioned and orientated actuator a
nd/or sensor layers. Use is made of the von Karman nonlinear strain-di
splacement relations. Subsequently, the static stability equations for
the initial (bifurcation) buckling under transverse and compressive l
oads are formulated via the Euler method of the adjacent equilibrium c
onfigurations. The present analysis is quite general in that no assump
tions are made on the placements of the active layers, their symmetry,
and their constitutive relations. The only assumptions pertain to the
behavior of the adaptive multilayered beam as one equivalent, linear
elastic, anisotropic beam (smeared laminate model). Numerical results
deal with the nonlinear flexural response of unsymmetrically laminated
beams under transverse and compressive axial loads. It is concluded t
hat the effectiveness of the control depends on the boundary condition
s, mechanisms of activation and lay-ups.