Given a 3-ply [0/60]s unidirectional aramid/epoxy laminate with a volume fraction of 60%subjected to loads Nx = 100 N/m and Mx = 50 N m/m. Assume each ply has a thickness of 5mm. Use the values calculated from HW #6 to determine the following:a. The three stiffness matrices [A], [B], and [D]b. The midplane strains and curvaturesc. The global and local stresses and strains on the top surface of the 60° ply.d. The in-plane and flexural stiffnesses of the laminatee. Apply Tsai-Hill Failure Criterion for the top surface of the 60° ply.f. Apply the Maximum Strain Failure Criterion for the top surface of the 60° ply.

The key steps in the analysis are:Calculating the laminate stiffness matrices [A], [B], and [D]…

Answered: Given a 3-ply [0/60]s unidirectional…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

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