steel tension test specimen has a diameter of 6.00 mm and a gage length of 25 mm. The following data are of id test: Load, KN 0 2.94 Deformation, mm 0 0.01 Tensile Test Result Load, KN 13.22 13.25 Deformation, mm 0.10 0.14 Load, KN 20.72 20.61

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Problem 1.5.6P: The data in Table 1.5.3 were obtained from a tensile test of a metal specimen with a rectangular...
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Explain in your own words how are these properties determined.

A steel tension test specimen has a diameter of 6.00 mm and a gage length of 25 mm. The following data are obtained from the
said test:
Tensile Test Result
Load, kN
Deformation, mm
Load, kN
Deformation, mm
Load, kN
Deformation, mm
13.22
0.10
20.72
3.36
2.94
0.01
13.25
0.14
20.61
3.83
5.58
0.02
13.22
0.17
20.27
3.94
8.52
0.03
13.22
0.29
19.97
4.00
11.16
0.04
16.15
0.61
19.68
4.06
12.63
0.05
18.50
1.04
19.09
4.12
13.02
0.06
20.27
1.80
18.72
fracture
13.16
0.08
20.56
2.26
13.22
0.08
20.67
2.78
Determine the material properties of the specimen and explain how are these parameters obtained.
Transcribed Image Text:A steel tension test specimen has a diameter of 6.00 mm and a gage length of 25 mm. The following data are obtained from the said test: Tensile Test Result Load, kN Deformation, mm Load, kN Deformation, mm Load, kN Deformation, mm 13.22 0.10 20.72 3.36 2.94 0.01 13.25 0.14 20.61 3.83 5.58 0.02 13.22 0.17 20.27 3.94 8.52 0.03 13.22 0.29 19.97 4.00 11.16 0.04 16.15 0.61 19.68 4.06 12.63 0.05 18.50 1.04 19.09 4.12 13.02 0.06 20.27 1.80 18.72 fracture 13.16 0.08 20.56 2.26 13.22 0.08 20.67 2.78 Determine the material properties of the specimen and explain how are these parameters obtained.
A Stress-Strain Curves
Back File
Force Deformation
Stress
Strain
Stress (MPa)
Zoom
x 2
(kN)
(mm)
(MPa)
(mm/mm)
1.
0.000
0.00000
750.
2.
2.94
103.997
0.00000
700.
3
5.58
0.01
197.382
400.00E-06
4
8.52
0.02
301.380
800.00E-06
650.
5.
11.16
0.03
394.765
0.001200
600.
6
13.02
0.04
460.559
0.001600
7
13.16
0.05
465.511
0.002000
550.
8
13.22
0.08
467.634
0.003200
500.
9
13.22
0.08
467.634
0.003200
450.
10
13.25
0.10
468.695
0.004000
11
13.22
0.14
467.634
0.005600
400.
12
13.22
0.17
467.634
0.006800
350.
Force Units
Length Units
Stress Units
Strain Units
300.
kN
mm
MPa
mm/mm
250.
Specimen
Gage Length
Plotting
200.
Number of
150.
Points
25.00
Plot
100.
25
Area
50.
28.27
Set
0.
proportional
limit at point
Area Units
V 0.2% Offset Method
-50.
-5. 0.
5.
mm2
10. 15. 20. 25. 30. 35. 40. 45. 50. 55. 60. 65. 70. 75. 80. 85.
Strain ( x0.001 mm/mm)
7
V 0.05% Offset Method
Summary
Ultimate Stress
The ultimate stress (also called the ultimate strength) of the material is the largest stress on the
stress-strain curve. From the test data given, the ultimate stress for this material is 732.933 MPa.
ultimate Stress
Proportional Limit
Elastic Modulus
0.20% Yield Stress
0.05% Yield Stress
Percent Elongation
732.933 MPa
465.511 MPa
279,737.666 MPa
468.262 MPa
Proportional Limit
The stress-strain curve for most materials has an initial region in which the material stress is linearly
related to the material strain. The proportional limit marks the uppermost stress on this linear
portion of the stress-strain curve. The proportional limit is a stress. For stresses above the
proportional limit, the stress-strain relationship is non-linear. The proportional limit is determined by
inspection of the stress-strain curve. Using data point 7, the proportional limit for this material is
465.803 MPa
0.0000 percent
Transcribed Image Text:A Stress-Strain Curves Back File Force Deformation Stress Strain Stress (MPa) Zoom x 2 (kN) (mm) (MPa) (mm/mm) 1. 0.000 0.00000 750. 2. 2.94 103.997 0.00000 700. 3 5.58 0.01 197.382 400.00E-06 4 8.52 0.02 301.380 800.00E-06 650. 5. 11.16 0.03 394.765 0.001200 600. 6 13.02 0.04 460.559 0.001600 7 13.16 0.05 465.511 0.002000 550. 8 13.22 0.08 467.634 0.003200 500. 9 13.22 0.08 467.634 0.003200 450. 10 13.25 0.10 468.695 0.004000 11 13.22 0.14 467.634 0.005600 400. 12 13.22 0.17 467.634 0.006800 350. Force Units Length Units Stress Units Strain Units 300. kN mm MPa mm/mm 250. Specimen Gage Length Plotting 200. Number of 150. Points 25.00 Plot 100. 25 Area 50. 28.27 Set 0. proportional limit at point Area Units V 0.2% Offset Method -50. -5. 0. 5. mm2 10. 15. 20. 25. 30. 35. 40. 45. 50. 55. 60. 65. 70. 75. 80. 85. Strain ( x0.001 mm/mm) 7 V 0.05% Offset Method Summary Ultimate Stress The ultimate stress (also called the ultimate strength) of the material is the largest stress on the stress-strain curve. From the test data given, the ultimate stress for this material is 732.933 MPa. ultimate Stress Proportional Limit Elastic Modulus 0.20% Yield Stress 0.05% Yield Stress Percent Elongation 732.933 MPa 465.511 MPa 279,737.666 MPa 468.262 MPa Proportional Limit The stress-strain curve for most materials has an initial region in which the material stress is linearly related to the material strain. The proportional limit marks the uppermost stress on this linear portion of the stress-strain curve. The proportional limit is a stress. For stresses above the proportional limit, the stress-strain relationship is non-linear. The proportional limit is determined by inspection of the stress-strain curve. Using data point 7, the proportional limit for this material is 465.803 MPa 0.0000 percent
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