A composite cantilever beam, made of high-strength (HS) carbon/epoxy material with [04/304]s plies, has uniformly applied load gO. When g0=50 N/m, length of the beam, L=0./ m, and width of the beam, b=0.05 m. Find the maximum deflection of the beam.
(for the HS carbon fiber/epoxy, £11 =131 GPa, £22 = 11.2 GPa, vl2 = 0.28, G12 = 6.55 GPa and ply thickness =0.2 mm).