The following data was collected from a tensile test and plotted on a copper-nickel alloy. The gage length after fracture was 2.75 in and the diameter at fracture was 0.365 in. From the plot above, what is the ultimate Tensile Strength? From the plot above, what is the Fracture Stress?

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The following data was collected from a tensile test and plotted on a copper-nickel alloy. The gage length after fracture was 2.75 in and the diameter at fracture was 0.365 in. From the plot above, what is the ultimate Tensile Strength? From the plot above, what is the Fracture Stress?
Engineering Stress (ksi)
60
50
40
30
20
10
0
0.00
0.05
S
UTS
e
0.10
UTS
| I
= 54.9 ksi
= 0.140
0.15
0.20
0.25
Engineering Strain
S
fracture
fracture
0.30
=
= 44.9 ksi
= 0.375
=
0.35
0.40
Transcribed Image Text:Engineering Stress (ksi) 60 50 40 30 20 10 0 0.00 0.05 S UTS e 0.10 UTS | I = 54.9 ksi = 0.140 0.15 0.20 0.25 Engineering Strain S fracture fracture 0.30 = = 44.9 ksi = 0.375 = 0.35 0.40
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