Case Study Determine Properties from Tensile Test Data A cylindrical specimen of stainless steel having an initial diameter of 12.8mm and initial length of 50.8mm is pulled in tension. Use the data provided below to a) Plot the data as engineering stress versus engineering strain using excel or similar software. 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. Load (N) Length (mm) 50.800 12,700 25,400 50.825 50.851 38,100 50,800 76,200 89,100 92,700 102,500 107,800 50.876 50.902 50.952 51.003 51.054 51.181 51.308 119,400 128,300 149,700 51.562 51.816 52.832 159,000 53.848 160,400 159,500 151,500 124,700 54.356 54.864 55.880 56.642 Fracture

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Case Study
Determine Properties from Tensile Test Data
A cylindrical specimen of stainless steel having an initial diameter of 12.8mm and initial length
of 50.8mm is pulled in tension. Use the data provided below to
a) Plot the data as engineering stress versus engineering strain using excel or similar
software.
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.
Load (N)
Length (mm)
50.800
12,700
25,400
38,100
50,800
76,200
50.825
50.851
50.876
50.902
50.952
89,100
92,700
51.003
51.054
102,500
107,800
119,400
128,300
149,700
159,000
160,400
159,500
151,500
124,700
51.181
51.308
51.562
51.816
52.832
53.848
54.356
54.864
55.880
56.642
Fracture
Transcribed Image Text:Case Study Determine Properties from Tensile Test Data A cylindrical specimen of stainless steel having an initial diameter of 12.8mm and initial length of 50.8mm is pulled in tension. Use the data provided below to a) Plot the data as engineering stress versus engineering strain using excel or similar software. 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. Load (N) Length (mm) 50.800 12,700 25,400 38,100 50,800 76,200 50.825 50.851 50.876 50.902 50.952 89,100 92,700 51.003 51.054 102,500 107,800 119,400 128,300 149,700 159,000 160,400 159,500 151,500 124,700 51.181 51.308 51.562 51.816 52.832 53.848 54.356 54.864 55.880 56.642 Fracture
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