A cantilever beam is subjected to a parabolically varying end shear stress resulting in a load of P N and a linearly distributed load p N/cm (Fig. P7.42). Dividing the beam into two triangles as shown, calculate the stresses in the member. The beam is made of a transversely isotropic material, in which a rotational symmetry of properties exists within the xz plane:
Here is associated with the behavior in the xz plane, and with the direction perpendicular to the xz plane. Now the elasticity matrix, Eq. (7.54), becomes
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