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Interacting Subsystems
                             different types of waves that we can effectively guide. Some of these sur-
                             face waves have special names:
                             • Beams: Flexural waves. (Daniel Bernoulli, 08/02/1700–17/03/1782,
                               Leonard Euler, 15/04/1707–1783, and Stephen P. Timoshenko, 22/12/
                               1878–29/05/1972).
                             • Homogeneous half-space: Rayleigh waves (John William Strutt Lord
                               Rayleigh, 12/11/1842–30/06/1919).

                             • Plates: Lamb waves (Horace Lamb, 29/11/1849–4/11/1934).
                             • Thin layer on an elastic half-space: Love waves (Augustus Edward
                               Hough Love, 17/04/1863–5/06/1940).

                             The basic analysis technique is to first make a unique decomposition of
                             the displacement field into two parts  u =  u′ +  u″  . One component is
                             divergence-free and the other is rotation-free. Because of this separation,
                                                                    φ
                             we can assume the existence of a scalar potential   and a vector potential
                             ψψ ψ ψ   (as we did for the electrodynamic potentials  ψ   and  A  ), and hence
                             obtain the unique decomposition
                                                u =  ∇× ψψ ψ ψ +  ∇ φ            (7.113)

                Elasticity for   The analysis is greatly simplified for the Lamb and Raleigh waves if we
                Raleigh and   choose the direction of propagation parallel to a coordinate axis, here the
                Lamb Waves
                                                                      u
                             x-axis. In addition, we assume no dependence of   on the y-direction
                             (for the plate this means a plane strain assumption), so that
                                   ,,
                             ψψ ψ ψ =  ( 0 ψ 0)   and hence
                                                            ------ 0 ------- +
                                                       ------- +
                                                                      ------
                                     u =  ( u 0 u,,  ) =   –  ∂ψ  ∂φ ,,  ∂ψ  ∂φ   (7.114)
                                           1    3     ∂z   ∂x   ∂x   ∂z 
                             From elasticity, we recall that the “small” strain is defined component-
                             wise as

                                                    1 ∂u  i  ∂u  j
                                                     
                                               ε =  --- -------- +  --------     (7.115)
                                                ij        ∂x 
                                                    2 ∂x  j  i


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