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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
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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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
Transcribed Image Text: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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