A small aluminum alloy [E = 74 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 130 mm. The cross-sectional dimensions of the tee shape are b = 25 mm, d = 38 mm, and t = 9 mm. After loads are applied to the beam at B, C, and D, acompressive normal strain of 460 µɛ is measured from a strain gage located at c = 5 mm below the topmost edge of the tee stem atsection 1-1. What is the applied load P?P3PStrain gage-dВDE2HAnswer:P= iN

Answered: Image /qna-images/answer/98e52b18-0203-4df7-bfde-2aa18abc115b.jpg

small aluminum alloy [E = 74 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 130 mm. The cross- ectional dimensions of the tee shape are b = 25 mm, d = 38 mm, and t = 9 mm. After loads are applied to the beam at B, C, and D, a ompressive normal strain of 460 µɛ is measured from a strain gage located at c= 5 mm below the topmost edge of the tee stem at ection 1-1. What is the applied load P? P P 3P Strain gage- d B D E H b nswer:

small aluminum alloy [E = 74 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 130 mm. The cross- ectional dimensions of the tee shape are b = 25 mm, d = 38 mm, and t = 9 mm. After loads are applied to the beam at B, C, and D, a ompressive normal strain of 460 µɛ is measured from a strain gage located at c= 5 mm below the topmost edge of the tee stem at ection 1-1. What is the applied load P? P P 3P Strain gage- d B D E H b nswer:

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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