A small aluminum alloy [E = 62 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 185 mm. The cross- sectional dimensions of the tee shape are b = 22 mm, d = 33 mm, and t = 7 mm. After loads are applied to the beam at B, C, and D, a compressive normal strain of 400 µe is measured from a strain gage located at c = 9 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P? P 3P | V Strain gage d H Answer: P= i 287.77 N 미2

Structural Analysis
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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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A small aluminum alloy [E = 62 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 185 mm. The cross-
sectional dimensions of the tee shape are b = 22 mm, d = 33 mm, and t = 7 mm. After loads are applied to the beam at B, C, and D, a
compressive normal strain of 400 µe is measured from a strain gage located at c = 9 mm below the topmost edge of the tee stem at
section 1-1. What is the applied load P?
P
3P
| V
Strain gage
d
H
Answer:
P= i
287.77
N
미2
Transcribed Image Text:A small aluminum alloy [E = 62 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 185 mm. The cross- sectional dimensions of the tee shape are b = 22 mm, d = 33 mm, and t = 7 mm. After loads are applied to the beam at B, C, and D, a compressive normal strain of 400 µe is measured from a strain gage located at c = 9 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P? P 3P | V Strain gage d H Answer: P= i 287.77 N 미2
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