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tesi R. Valiante.pdf - EleA@UniSA

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40<br />

ν =<br />

2<br />

λ<br />

( λ + µ )<br />

(1.40b)<br />

To well-define the problem of Lamb waves in plates, boundary conditions<br />

must be applied at both free surfaces of the plate. On these surfaces the traction<br />

must vanish. Moreover, the assumption of plain stress must be done. Under these<br />

conditions, it is possible to find a solution to Eq.1.39, which describes Lamb<br />

waves in a homogeneous plate. To solve this problem, the method of the<br />

displacements potentials can be used [35]. The solution can be split into two<br />

parts with symmetric and anti-symmetric properties. Each part leads to a<br />

different Lamb wave mode, one symmetric and one anti-symmetric, as<br />

expressed in Eq.1.41,<br />

tan<br />

tan<br />

( qh)<br />

2<br />

4k<br />

qp<br />

= −<br />

(1.41a)<br />

k − q<br />

( ) ( ) 2<br />

ph<br />

2 2<br />

( qh)<br />

( ph)<br />

2 2 ( k q )<br />

2<br />

tan −<br />

= −<br />

(1.41b)<br />

2<br />

tan 4k<br />

qp<br />

where p and q are defined in Eq.1.42,<br />

p<br />

q<br />

2<br />

2<br />

2<br />

= − k<br />

c<br />

ω<br />

2<br />

L<br />

2<br />

= − k<br />

c<br />

ω<br />

2<br />

T<br />

2<br />

2<br />

(1.42a)<br />

(1.42b)<br />

and h, k and ω are the half-thickness of the plate, wavenumber and<br />

frequency respectively. The graphical representation of the symmetric and the<br />

anti-symmetric modes is shown in Fig.1.14, the arrows represent the<br />

displacements of the material. Equations Eq.1.41 can be solved analytically just

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