Response to the following problem:
Given the following stresses
σx = Ak z sin (αx) sin (βy)
σy = Bk z sin (αx) sin (βy)
σxy = 0
σyz = Qk sin (αx) cos (βy)
σxz = Rk cos (αx) sin (βy)
Where k = 1 . . . N, N is the number of laminae, and Ak, Bk, Qk, and R are constants, derive the seven stress resultants integrating over the thickness of a laminated plate with N = 3, t1 = t2 = t3.