A composite beam is made of two brass [E = 96 GPa] plates bonded to an aluminum [E = 62 GPa] bar, as shown. The beam is subjected to a bending moment of 2260 N-m acting about the z axis. Assume b=53 mm, d;=48 mm, dz=14 mm. Determine: (a) the maximum bending stresses o,. Gu in the brass plates and the aluminum bar. (b) the stress in the brass ouj at the joints where the two materials are bonded together. Brass (2) di Aluminum (1) Brass (2)

Structural Analysis
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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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A composite beam is made of two brass [E = 96 GPa] plates bonded to an aluminum [E = 62 GPa] bar, as shown. The beam is subjected to a bending moment of 2260 N-m acting about the z axis. Assume b=53 mm, d1=48 mm, d2=14 mm. Determine:
(a) the maximum bending stresses σbrσb⁢r, σalσa⁢l in the brass plates and the aluminum bar.
(b) the stress in the brass σbrjσb⁢r⁢j at the joints where the two materials are bonded together.

A composite beam is made of two brass [E = 96 GPa] plates bonded to an aluminum [E = 62 GPa] bar, as shown. The beamis subjected
to a bending moment of 2260 N-m acting about the z axis. Assume b=53 mm, d;=48 mm, dz=14 mm. Determine:
(a) the maximum bending stresses oy. Ga in the brass plates and the aluminum bar.
(b) the stress in the brass oj at the joints where the two materials are bonded together.
Brass (2)
dz
d
Aluminum (1)
Brass (2)
Answers:
(a) opr =
MPa, oa =
MPa.
(b) σ-
MPa.
Transcribed Image Text:A composite beam is made of two brass [E = 96 GPa] plates bonded to an aluminum [E = 62 GPa] bar, as shown. The beamis subjected to a bending moment of 2260 N-m acting about the z axis. Assume b=53 mm, d;=48 mm, dz=14 mm. Determine: (a) the maximum bending stresses oy. Ga in the brass plates and the aluminum bar. (b) the stress in the brass oj at the joints where the two materials are bonded together. Brass (2) dz d Aluminum (1) Brass (2) Answers: (a) opr = MPa, oa = MPa. (b) σ- MPa.
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