Compute the stresses σx and σ1 in the 45? and in the -45? laminae right next to the interface based on the strains computed in Exercise 1 using (6.24). Discuss the results.
Exercise 1
Compute the strains ∈x, ∈y, and γxy at the interface between the 45° and -45° laminae above the middle surface by using the results of case (b) of Exercise 2 and (6.23).
Exercise 2
Consider a [+45/ - 45]S laminate with the material properties of Exercise. Compute the middle-surface strain ∈0x, ∈0y, γ0xy
and the curvatures κx, κy, κxy for the following load cases
(a) Nx = 1000 N/m; all remaining components are equal to zero
(b) Mxy = 1 Nm/m; all remaining components are equal to zero
(c) Comment on the coupling effects observed.