= An orthotropic fibrous composite (Xt = Xc = 800, Ye Yt = 1400MPa, E =...

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= An orthotropic fibrous composite (Xt = Xc = 800, Ye Yt = 1400MPa, E = 320GPa, E2 = 80GPa, V12 = 0.3, V21 = 0.35, G12 0.35, G12 = 60GPa) is under the following loading. The angle of the fibers with the x-axis is 15. a) Find the tensile and shear strains in the x and y directions at the point with maximum tensile stress in the x direction. (plane stress assumption is considered) b) Check if the material will fail under the given loading using the maximum stress theory. c) Solve the problem using ANSYS software and compare your results. www 30mm 20mm 3 m L. 12 kN/m B = -1.5 m V(KN) 16.5 1-375 9.00 3 -19.5 +-x(m) M(KN-m) 11-34 A 1-375 -4-50 -X (m) = An orthotropic fibrous composite (Xt = Xc = 800, Ye Yt = 1400MPa, E = 320GPa, E2 = 80GPa, V12 = 0.3, V21 = 0.35, G12 0.35, G12 = 60GPa) is under the following loading. The angle of the fibers with the x-axis is 15. a) Find the tensile and shear strains in the x and y directions at the point with maximum tensile stress in the x direction. (plane stress assumption is considered) b) Check if the material will fail under the given loading using the maximum stress theory. c) Solve the problem using ANSYS software and compare your results. www 30mm 20mm 3 m L. 12 kN/m B = -1.5 m V(KN) 16.5 1-375 9.00 3 -19.5 +-x(m) M(KN-m) 11-34 A 1-375 -4-50 -X (m)

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The image shows a problem statement with an accompanying diagram of a cantilevered beam and its shear force V and bending moment M diagrams The proble... View the full answer