Given the following stresses
σx = Akz sin(αx) sin(βy)
σy = Bkz 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 Rk are constants, derive the seven stress resultants integrating over the thickness of a laminated plate with N = 3, t1 = t2 = t3.