A small aluminum alloy [E = 75 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 160 mm. The cross- sectional dimensions of the tee shape are b = 21 mm, d= 32 mm, and t = 4 mm. After loads are applied to the beam at B, C, and D, a compressive normal strain of 460 µɛ is measured from a strain gage located at c = 7 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P?
A small aluminum alloy [E = 75 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 160 mm. The cross- sectional dimensions of the tee shape are b = 21 mm, d= 32 mm, and t = 4 mm. After loads are applied to the beam at B, C, and D, a compressive normal strain of 460 µɛ is measured from a strain gage located at c = 7 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P?
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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![A small aluminum alloy [E = 75 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 160 mm. The cross-
sectional dimensions of the tee shape are b = 21 mm, d= 32 mm, and t = 4 mm. After loads are applied to the beam at B, C, and D, a
compressive normal strain of 460 µɛ is measured from a strain gage located at c = 7 mm below the topmost edge of the tee stem at
section 1-1. What is the applied load P?
P
P
ЗР
C
Strain gage-
d
E
H
b
Answer:
P = i
N
/2](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F0fae10eb-699d-4206-941e-42e55c1a7413%2F9640921b-4901-4cac-9870-90dc7698967b%2Fwwxyaolb_processed.jpeg&w=3840&q=75)
Transcribed Image Text:A small aluminum alloy [E = 75 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 160 mm. The cross-
sectional dimensions of the tee shape are b = 21 mm, d= 32 mm, and t = 4 mm. After loads are applied to the beam at B, C, and D, a
compressive normal strain of 460 µɛ is measured from a strain gage located at c = 7 mm below the topmost edge of the tee stem at
section 1-1. What is the applied load P?
P
P
ЗР
C
Strain gage-
d
E
H
b
Answer:
P = i
N
/2
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