Consider an angle-ply laminated shell (i.e. [±45]s laminate) made from plies of unidirectional… 1 answer below »

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Consider an angle-ply laminated shell (i.e. [±45]s laminate) made from plies of

unidirectional carbon-epoxy fiber composite material.

The engineering properties for each ply in local lamina coordinates are given

below (L = longitudinal and T = transverse) :

Mechanical properties: =143 Gpa, =10.1 Gpa; =4.14 Gpa, =0.31

Hygro-mechanical swelling coefficients: ßL = 0 / % wt, ßT = 6.67E-3 / % wt

Find the following effective properties of this angle-ply laminate in global XY

laminate coordinates:

a) In plane Young’s moduli Ex and Ey,

b) In-plane shear modulus

c) In-plane Poisson’s ratio

d) In-plane hygromechanical expansion coefficients ßX and ßY

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