Finite Element Multidisciplinary Analysis, Second Edition

A one-dimensional beam element with six displacement degrees of freedom at each node is shown in Fig. 4.1. Structural characteristics of the straight element with uniform cross section A may be obtained from assumed axial, torsional, and flexural deformation components, combining these individual relationships as described next. [1] , [2] The local coordinate system is assumed such that the x axis corresponds to the axial direction of the element. The six displacement degrees of freedom at any point on the element are shown in Fig. 4.1.
Thus for the axial element the displacement interpolation in the local x direction assumes a linear relationship:
The coefficients c 1 and c 2 are evaluated in terms of nodal displacements by setting the boundary conditions u x = u x1 at x = 0 and u x = u x2 at x = l, so that
where N is the shape function row vector pertaining to the x direction. The strain is given by differentiation of u x with respect to x,
and the stiffness and inertia matrices are obtained as
using Eqs. (3.59) and (3.61) derived in Chapter 3. In these equations, E is the Young's modulus of elasticity, ? the mass density, A the area of the beam cross section, and l the length of the beam element.
For a...