****USE MATLAB TO SOLVE

THIS

QUESTION****

5. A composite cantilever beam, made of High Strength (HS) carbon/epoxy material

with [04/304], plies, has uniformly applied load qo. When qo-50N/m, length of the

beam, L=0.1m, and width of the beam, b=0.05m. Find the maximum deflection of

the beam.

(for the HS carbon fiber/epoxy, E₁1 =131 GPa, E22= 11.2 GPa, V12 = 0.28, G₁2 = 6.55 GPa

and ply thickness t=0.2mm)

90-50N/m

L