6. The following data were collected from a 12-mm diameter test specimen of magnesium (lo = 30.00 mm). After fracture, the total length was 32.61 mm and the diameter was 11.74 mm. Load Al (N) (mm) 0.0000 5,000 10,000 15,000 20,000 25,000 26,500 0.0296 0.0592 0.0888 0.15 0.51 0.90 27,000 1.50 (maximum load) 26,500 2.10 25,000 2.79 (fracture) a) Plot the data as engineering stress versus engineering strain. b) Compute the modulus of elasticity. c) Determine the yield strength at a strain offset of 0.002. d) Determine the tensile strength of this alloy. e) What is the approximate ductility, in percent elongation? f) Compute the modulus of resilience. g) Compute from the data and plot true stress versus true strain diagram.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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6. The following data were collected from a 12-mm diameter test specimen of
magnesium (lo = 30.00 mm). After fracture, the total length was 32.61 mm and
the diameter was 11.74 mm.
Load
(N)
Al
(mm)
0.0000
5,000
10,000
15,000
20,000
25,000
26,500
0.0296
0.0592
0.0888
0.15
0.51
0.90
1.50 (maximum load)
2.10
2.79 (fracture)
27,000
26,500
25,000
a)
Plot the data as engineering stress versus engineering strain.
b)
Compute the modulus of elasticity.
c)
Determine the yield strength at a strain offset of 0.002.
d)
Determine the tensile strength of this alloy.
e)
What is the approximate ductility, in percent elongation?
f)
Compute the modulus of resilience.
g)
Compute from the data and plot true stress versus true strain diagram.
Transcribed Image Text:6. The following data were collected from a 12-mm diameter test specimen of magnesium (lo = 30.00 mm). After fracture, the total length was 32.61 mm and the diameter was 11.74 mm. Load (N) Al (mm) 0.0000 5,000 10,000 15,000 20,000 25,000 26,500 0.0296 0.0592 0.0888 0.15 0.51 0.90 1.50 (maximum load) 2.10 2.79 (fracture) 27,000 26,500 25,000 a) Plot the data as engineering stress versus engineering strain. b) Compute the modulus of elasticity. c) Determine the yield strength at a strain offset of 0.002. d) Determine the tensile strength of this alloy. e) What is the approximate ductility, in percent elongation? f) Compute the modulus of resilience. g) Compute from the data and plot true stress versus true strain diagram.
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