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Plate and Shell Analyses                                                    193



            and

                                                                    ∂θ 
                             ε= z  ∂θ y  ,  ε= − z  ∂θ x  ,  γ xy  = z  ∂θ y  −  x  ,
                                          y
                              x
                                                                       x
                                   ∂x             ∂y             ∂y  ∂  
                                                                                       (6.18)
                                  ∂w              ∂w
                             γ xz  =  +θ y ,  γ yz =  −θ x
                                               z
                                   ∂x              ∂ y
              Note that if we impose the conditions (or assumptions) that
                                       ∂w                 ∂w
                                     =     +θ = 0,      =     −θ = 0                   (6.19)
                                  γ xz        y      γ yz        x
                                       ∂x                 ∂y
            then we can recover the relations applied in the thin plate theory.
              The governing equations and boundary conditions can be established for thick plates
            based on the above assumptions, with the three main variables involved being w(x, y),
            θ (x, y), and θ (x, y).
                        y
             x
            6.2.4  Shell Theory
            Unlike the plate models, where only bending forces exist, there are two types of forces in
            shells, that is, membrane forces (in plane forces) and bending forces (out of plane forces)
            (Figures 6.8 and 6.9).


            6.2.4.1  Shell Example: A Cylindrical Container
            Similar to the plate theories, there are two types of theories for modeling shells, namely
            thin shell theory and thick shell theory. Shell theories are the most complicated ones to
            formulate and analyze in mechanics. Many of the contributions were made by Russian
            scientists in the 1940s and 1950s, due to the need to develop new aircrafts and other light-
            weight structures. Interested readers can refer to Reference [6] for in-depth studies on this
            subject. These theoretical works have laid the foundations for the development of various
            finite elements for analyzing shell structures.




















            FIGURE 6.8
            Forces and moments in a shell structure member.
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