Question: For Example 16.1, show that the element stiffness equations for the isotropic case are given by relations (16.4.1) and (16.4.2). Data from example 16.1 Equation

For Example 16.1, show that the element stiffness equations for the isotropic case are given by relations (16.4.1) and (16.4.2).

Data from example 16.1

Consider the plane stress problem of an isotropic elastic plate under uniform tension with zero body forces,

y 4 3 1 1 (2) 2 3 3 2 2 T -X

The element mesh is labeled as shown with local node numbers within each element and global node numbers

In similar fashion for element 2, 61 = 0, B2 = 1, B3 =  1, y1 = -1, Y2 = 0, Y3 = 1, A1 = 1/2, and the element

These individual element equations are to be assembled to model the plate, and this is carried out using the

K+K KQ+K2 K KQ K+K K(! +K() K!! K(!) K16 K +K(2) K + K K K K K 33 K34 (1) 44 K+K 35 (1) K56 (1) U1 V U V U3

where U, and V; are the global x and y nodal displacements, and K and K are the local stiffness components

Equation 16.4.1

E 2(1-1) [1 0 -1 -V 1-v V 0  V   . 0 V -1 0 3 (1) 4 (1) 1x ly 2x !!! TO) (16.4.1)

Equation 16.4.2

E 2(1-1)  O 1 -V -  0 1 0 1 - v 2  V -1  3-v 1 - -1 V |2 3-P 2 (2) (2) Wi (2) (2) uz Co (2) 2x IM (16.4.2)

Consider the plane stress problem of an isotropic elastic plate under uniform tension with zero body forces, as shown in Fig. 16.3. For convenience, the plate is taken with unit dimensions and thickness and is discretized into two triangular elements as shown. This simple problem is chosen in order to demonstrate some of the basic FEM solution procedures previously presented. More complex examples are discussed in the next section to illustrate the general power and utility of the numerical technique.

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