Using the material properties in Example 3.16, determine the residual thermal stresses in each…

Using the material properties in Example 3.16, determine the
residual thermal stresses in each lamina of (i) a [902=0]S and (ii) a [0=90=0]S
laminate. Both laminates are slowly cooled down from a curing temperature of
1908C to 238C.

Example 3.6