b. The simply supported beam shown in Figure 9 is fabricated by bonding four separate layers of a fiber reinforced composite with an industrial adhesive. The length of the beam is L=2 m, and the thickness and width of each lamina is %=25 mm and w=50 mmrespectively. The thickness of the adhesive may be neglected. A centrally concentrated load P=10 kNis applied to the beam. Upon applying a Factor of Safety of 2.5, determine the minimum shear strength of the adhesive to prevent delamination. Using a sketch, indicate which layer is most prone to failure because of the shearing stresses.

Mechanics of Materials (MindTap Course List)
9th Edition
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
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Chapter1: Tension, Compression, And Shear
Section: Chapter Questions
Problem 1.9.6P: A steel pad supporting heavy machinery rests on four short, hollow, cast iron piers (see figure)....
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b. The simply supported beam shown in Figure 9 is fabricated by bonding four separate layers of a
fiber reinforced composite with an industrial adhesive. The length of the beam is L=2 m, and the
thickness and width of each lamina is = 25 mmand w=50 mmrespectively. The thickness of the
adhesive may be neglected. A centrally concentrated load P=10 kNis applied to the beam. Upon
applying a Factor of Safety of 2.5, determine the minimum shear strength of the adhesive to prevent
delamination. Using a sketch, indicate which layer is most prone to failure because of the shearing
stresses.
P,
Adhesive
t
L/2
L/2
Transcribed Image Text:b. The simply supported beam shown in Figure 9 is fabricated by bonding four separate layers of a fiber reinforced composite with an industrial adhesive. The length of the beam is L=2 m, and the thickness and width of each lamina is = 25 mmand w=50 mmrespectively. The thickness of the adhesive may be neglected. A centrally concentrated load P=10 kNis applied to the beam. Upon applying a Factor of Safety of 2.5, determine the minimum shear strength of the adhesive to prevent delamination. Using a sketch, indicate which layer is most prone to failure because of the shearing stresses. P, Adhesive t L/2 L/2
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