Compute the stresses sigmax and sigma1 in the 45 and in the


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.

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