Question: For the beam problem in Example 8.3, the boundary conditions required that the resultant normal force vanish at each end (x = l). Show, however,

For the beam problem in Example 8.3, the boundary conditions required that the resultant normal force vanish at each end (x =± l). Show, however, that the normal stress on each end is not zero, and plot its distribution over –c

Data from example 8.3

Our final example in this section is that of a beam carrying a uniformly distributed transverse loading w

wl 2c Ty 21 W W X

It is noted that the fifth-order term has been generated to satisfy the biharmonic equation. The resulting

This completes determination of the four constants in the trial Airy stress function. The problem is nowThe corresponding results from strength of materials for this case (see Appendix D, Section D.3) are given by

Dimensionless Stress 15 10 5 dr -10 -15 -1 V/c = 2 V/c = 3 V/c = 4 a/w - Elasticity o/W-Strength of Materials

Next let us determine the displacement field for this problem. As in the previous examples, the displacements

Choosing the fixity conditions u(0,y) = v(1,0) = 0, the rigid-body motion terms are found to be 12/4 Up = Wo


Our final example in this section is that of a beam carrying a uniformly distributed transverse loading w along its top surface, as shown in Fig. 8.3. Again, plane stress conditions are chosen, and we relax the boundary conditions on the ends and consider only statically equivalent effects. Exact pointwise boundary conditions will be specified on the top and bottom surfaces, while at the ends the resultant horizontal force and moment are set to zero and the resultant vertical force will be specified to satisfy overall equilibrium. Thus, the boundary conditions on this problem can be written as Txy(x, c) = 0 a, (x,c) = 0 oy(x, -c) = -w Last: ox(l, y)dy = 0 0,(1, y)ydy = 0 (8.1.24) try (1, y)dy = Fwl Again, it is suggested that these conditions be verified, especially the last statement. Using the polynomial solution format, we choose a trial Airy stress function including second-, third-, and fifth-order terms (a choice that has come from previous trial and error) = A20x + A21xy + A03y + A23xy 423,5 (8.1.25)

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