Issue 41
M.F. Funari et alii, Frattura ed Integrità Strutturale, 41 (2017) 524-535; DOI: 10.3221/IGF-ESIS.41.63
0 T U W
(1)
where T is the virtual work of the inertial forces, U
is the work of the internal forces and the tractions across the
interfaces and W is the work of the external forces. According to the first-order transverse shear deformable laminate theory and multilayered approach, the variational form of the governing equations can be expressed by means of the following expressions: 1 2 0 1 2 l LN l l l l l l l l T U U dx, U U
1 0
l
L
L N
1
N
l
i
0
0
i T dX , i
l l l U N T M dx l l l
(2)
1
1
l
i
L
L
N
N
l
l
0
0
W f U h dX p U dx
l
l l
l
l
1
1
l
l
where the subscripts l=1,..,N and i=1,..,N-1 indicate the numbering of the layers ( N ) and the interfaces ( N-1 ), N,T ,M are the generalized stresses defined as a function of the classical extensional A , bending D , bending–extensional coupling D and the shear stiffness H variables, i t n T T T is the cohesive interfaces traction vector , i t n is the cohesive interface displacement jump vector, and 0 are the mass and polar mass per unit length of the layer and l f and l p ,with 1 2 0 l f f f and 1 2 l p p p m , are the per unit volume and area forces acting on the l -th layer, respectively. , , with 1 1 U , 2 U , ' ' ' ,x represent the generalized strains,
Figure 1 : Layered structure: geometry, interfaces and TSL
526
Made with FlippingBook Ebook Creator