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194                   Finite Element Modeling and Simulation with ANSYS Workbench







                                        p                                p





                                  Internal forces:




                                                                        p
                                                p
                                                                   Membrane stresses
                                                                      dominate


            FIGURE 6.9
            Internal forces acting in a cylinder under internal pressure load.




            6.3  Modeling of Plates and Shells

            Plates or shells can be modeled as flat or curved surfaces in space, with the thickness t
            assigned as a parameter (Figure 6.10). Discretization of the surfaces will involve the use
            of plate or shell elements, with the quality of the surface mesh improving with decreasing
            element size.
              Figure 6.11 gives an example of a stamping part analyzed using shell elements. The
            bracket has a uniform thickness and is fixed at the four bolt hole positions. A load is
            applied through a pin passing through the two holes in the lower part of the bracket. Note
            that one layer of elements on the edge of each hole has been masked in the stress contour
            plot (Figure 6.11b), due to inaccurate stress results near the constraint locations. To reduce
            the true stress levels in the bracket, the thickness can be changed, the shape of the bracket
            can be modified, and the model is remeshed and reanalyzed, all of which are very easy to
            carry out with the shell elements.
              In many cases, however, the plate and shell models may not be adequate for analyzing a
            structure member, even if it is considered thin. For example, the structure component has
            a nonuniform thickness (turbine blades, vessels with stiffeners, thin layered structures,
            etc.), see Figure 6.12, or has a crack for which detailed stress analysis is needed. In such









                                                              t

            FIGURE 6.10
            A shell structure member and its mathematical representation.
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