“…where = 11 is the extension stress, = 55 , is the shear stress, is the beam width, is the distance measured between the plane of the structure and that of the th layer laminate, ℎ is the total thickness of the structure (beam + actuator/sensor + beam), is the axial force, is the bending moment, is the shear force, 11 , 11 , 11 , 55 are the extension, extension-bending, bending, and transverse shear stiffness coefficients given by [13,15] …”