Find expressions for the moments (M_{x^{prime}} M_{y^{prime}}) and (M_{x y}) and the stresses (left(sigma_{x} ight)_{k^{prime}}left(sigma_{y} ight)_{k^{prime}}) and

Find expressions for the moments \(M_{x^{\prime}} M_{y^{\prime}}\) and \(M_{x y}\) and the stresses \(\left(\sigma_{x}\right)_{k^{\prime}}\left(\sigma_{y}\right)_{k^{\prime}}\) and \(\left(\tau_{x y}\right)_{k}\) in the \(k\) th ply of the uniformly loaded, specially orthotropic laminate with simply supported edges shown in Figure 7.48.

Transcribed Image Text:

q(x, y) x Simple supports on all edges FIGURE 7.48 Simply supported, specially orthotropic plate with distributed loading.