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A composite section will be used to support a heavy axial load of P-600 kN with a rigid plate at the top of the section. Determine the average compressive stress in the aluminum section. Use h=10 mm. Answer in MegaPascals. Brass core (E = 105 GPa) Rigid end plate %3D Aluminum plates (E = 70 GPa) %3D 300 mm 60 mm 40 mm None of these O 125 O 217.39 O 181.82 O 200

A composite section will be used to support a heavy axial load of P-600 kN with a rigid plate at the top of the section. Determine the average compressive stress in the aluminum section. Use h=10 mm. Answer in MegaPascals. Brass core (E = 105 GPa) Rigid end plate %3D Aluminum plates (E = 70 GPa) %3D 300 mm 60 mm 40 mm None of these O 125 O 217.39 O 181.82 O 200

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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A composite section will be used to support a heavy axial load of P-600 kN with a rigid plate at the top of the section. Determine the average compressive stress in the aluminum section. Use h=10 mm. Answer in MegaPascals. Brass core (E = 105 GPa) Rigid end plate %3D Aluminum plates (E = 70 GPa) %3D 300 mm 60 mm 40 mm None of these O 125 O 217.39 O 181.82 O 200
Transcribed Image Text:A composite section will be used to support a heavy axial load of P-600 kN with a rigid plate at the top of the section. Determine the average compressive stress in the aluminum section. Use h=10 mm. Answer in MegaPascals. Brass core (E = 105 GPa) Rigid end plate %3D Aluminum plates (E = 70 GPa) %3D 300 mm 60 mm 40 mm None of these O 125 O 217.39 O 181.82 O 200
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