The following data were obtained during a tension test of an aluminum alloy. The initial diameter of the test specimen was 0.505 in. and the gage length was 2.0 in. Load (lb) 0 2310 4 640 6 950 9 290 11 600 12 600 Elongation (in.) 0 0.00220 0.00440 0.00660 0.00880 0.0110 0.0150 Load (lb) 14 000 14 400 14 500 14 600 14 800 14 600 13 600 Elongation (in.) 0.020 0.025 0.060 0.080 0.100 0.120 Fracture

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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The following data were obtained during a tension
test of an aluminum alloy. The initial diameter of the
test specimen was 0.505 in. and the gage length was
2.0 in.
Load
(lb)
-O
2 310
4 640
6 950
9 290
11 600
12 600
Elongation
(in.)
O
0.00220
0.00440
0.00660
0.00880
0.0110
0.0150
Load
(lb)
14 000
14 400
14 500
14 600
14 800
14 600
13 600
Elongation
(in.)
0.020
0.025
0.060
0.080
0.100
0.120
Fracture
determine the
Plot the stress-strain diagram and
(a) proportional
following mechanical properties:
limit; (b) modulus of elasticity; (c) yield point;
yield strength at 0.2% offset;
and (f) rupture strength.
(d)
(e) ultimate strength;
Transcribed Image Text:The following data were obtained during a tension test of an aluminum alloy. The initial diameter of the test specimen was 0.505 in. and the gage length was 2.0 in. Load (lb) -O 2 310 4 640 6 950 9 290 11 600 12 600 Elongation (in.) O 0.00220 0.00440 0.00660 0.00880 0.0110 0.0150 Load (lb) 14 000 14 400 14 500 14 600 14 800 14 600 13 600 Elongation (in.) 0.020 0.025 0.060 0.080 0.100 0.120 Fracture determine the Plot the stress-strain diagram and (a) proportional following mechanical properties: limit; (b) modulus of elasticity; (c) yield point; yield strength at 0.2% offset; and (f) rupture strength. (d) (e) ultimate strength;
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