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2




            Bars and Trusses












            2.1  Introduction
            This chapter introduces you to the simplest one-dimensional (1-D) structural element,
            namely the bar element, and the FEA of truss structures using such element. Trusses
            are commonly used in the design of buildings, bridges, and towers (Figure 2.1). They are
            triangulated frameworks composed of slender bars whose ends are connected through
            bolts, pins, rivets, and so on. Truss structures create large, open, and uninterrupted space,
            and offer lightweight and economical solutions to many engineering situations. If a truss,
            along with the applied load, lies in a single plane, it is called a planar truss. If it has mem-
            bers and joints extending into the three-dimensional (3-D) space, it is then a space truss.
              Most structural analysis problems such as stress and strain analysis can be treated as
            linear static problems, based on the following assumptions:

              1.  Small deformations (loading pattern is not changed due to the deformed shape)
              2.  Elastic materials (no plasticity or failures)
              3.  Static loads (the load is applied to the structure in a slow or steady fashion)

              Linear analysis can provide most of the information about the behavior of a structure,
            and can be a good approximation for many analyses. It is also the basis of nonlinear FEA
            in most of the cases. In Chapters 2 through 7, only linear static responses of structures are
            considered.






            2.2  Review of the 1-D Elasticity Theory
            We begin by examining the problem of an axially loaded bar based on 1-D linear elasticity.
            Consider a uniform prismatic bar shown in Figure 2.2. The parameters L, A, and E are the
            length, cross-sectional area, and elastic modulus of the bar, respectively.
              Let u, ε, and σ be the displacement, strain, and stress, respectively (all in the axial direc-
            tion and functions of x only), we have the following basic relations:

              Strain–displacement relation:

                                                    du ()
                                                       x
                                                x
                                              ε()  =                                    (2.1)
                                                     dx
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