A small aluminum alloy [E = 65 GPa] tee shape is used as a simply supported beam as shown. For this beam, a-165 mm. The cross- sectional dimensions of the tee shape are b 19 mm, d 29 mm, and t 7 mm, After loads are applied to the beam at B, C, and D, a compressive normal strain of 480 uɛ is measured from a strain gage located at c 5 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P? 3P Strain gage a H. b. Answer: P =
A small aluminum alloy [E = 65 GPa] tee shape is used as a simply supported beam as shown. For this beam, a-165 mm. The cross- sectional dimensions of the tee shape are b 19 mm, d 29 mm, and t 7 mm, After loads are applied to the beam at B, C, and D, a compressive normal strain of 480 uɛ is measured from a strain gage located at c 5 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P? 3P Strain gage a H. b. Answer: P =
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![A small aluminum alloy [E 65 GPa] tee shape is used as a simply supported beam as shown. For this beam, a 165 mm. The cross-
sectional dimensions of the tee shape are b 19 mm, d= 29 mm, and t 7 mm, After loads are applied to the beam at B, C, and D,a
compressive normal strain of 480 uɛ is measured from a strain gage located at c=5 mm below the topmost edge of the tee stem at
section 1-1. What is the applied load P?
17
P.
P.
3P
Strain gage
D
a -
H.
a
b.
Answer:
! N
P = i
2.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F6aca6c43-03c6-442f-a653-8e77a8bb391f%2F565ab5a7-73ed-421d-8260-46f6797a9b90%2F0885cb9k_processed.jpeg&w=3840&q=75)
Transcribed Image Text:A small aluminum alloy [E 65 GPa] tee shape is used as a simply supported beam as shown. For this beam, a 165 mm. The cross-
sectional dimensions of the tee shape are b 19 mm, d= 29 mm, and t 7 mm, After loads are applied to the beam at B, C, and D,a
compressive normal strain of 480 uɛ is measured from a strain gage located at c=5 mm below the topmost edge of the tee stem at
section 1-1. What is the applied load P?
17
P.
P.
3P
Strain gage
D
a -
H.
a
b.
Answer:
! N
P = i
2.
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