6–123. Segment A of the composite beam is made from 2014-T6 aluminum alloy and segment B is A-36 steel. The allowable bending stress for the aluminum and steel are (oallow)al = 15 ksi and (ơ allow)st = 22 ksi. Determine the maximum allowable intensity w of the uniform distributed load. -15 ft- А 3 in. 3 in. 3 in. B.

6–123. Segment A of the composite beam is made from 2014-T6 aluminum alloy and segment B is A-36 steel. The allowable bending stress for the aluminum and steel are (oallow)al = 15 ksi and (ơ allow)st = 22 ksi. Determine the maximum allowable intensity w of the uniform distributed load. -15 ft- А 3 in. 3 in. 3 in. B.

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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Concept explainers

Composite Construction

Composite construction is the construction of structures in which two or more materials are used. Regarding structural engineering, composite construction is a construction where two materials are bound together in a technical manner such that both the materials act as a single unit to carry and transfer the load. The motives of composite construction are to increase the structural strength, make structures more aesthetic, and provide a sustainable environment.

Question

6–123. Segment A of the composite beam is made from
2014-T6 aluminum alloy and segment B is A-36 steel.
The allowable bending stress for the aluminum and steel
are (oallow)al = 15 ksi and (ơallow)st
the maximum allowable intensity w of the uniform
distributed load.
= 22 ksi. Determine
15 ft
A
3 in.
В
3 in.
3 in.
Probs. 6–122/123

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