A 10-mm-diameter bar of 1040 carbon steel (see Table 6.1) is subjected to a tensile load of 50,000 N, taking it beyond its yield point. Calculate the elastic recovery that would occur upon removal of the tensile load.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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Tensile Test Data for Some Typical Metal Alloys
Percent
Y.S.
[MPa (ksi)|
E
T.S.
[MPa (ksi)]
elongation
at failure
Alloy*
[GPa (psi)]
1. 1040 carbon steel
2. 8630 low-alloy steel
3. a. 304 stainless steel
b. 410 stainless steel
4. L2 tool steel
5. Ferrous superalloy (410)
6. a. Ductile iron, quench
b. Ductile iron, 60–40–18
200 (29 × 10)
600 (87)
680 (99)
205 (30)
700 (102)
1,380 (200)
700 (102)
580 (84)
329 (48)
145 (21)
416 (60)
220 (32)
83 (12)
827 (120)
825 (120)
320 (46.4)
750 (109)
800 (116)
515 (75)
800 (116)
1,550 (225)
800 (116)
750 (108)
461 (67)
150 (22)
457 (66)
290 (42)
150 (22)
862 (125)
895 (130)
652 (94.5)
17
22
193 (28 × 10)
200 (29 х 10)
40
22
12
22
200 (29 × 10)
165 (24 x 10)
169 (24.5 × 10)
70 (10.2 × 10°)
70.3 (10.2 × 10)
45 (6.5 x 10)
45 (6.5 × 10°)
107–110 (15.5–16 × 10')
110 (16 x 10)
110 (16.1 × 10)
9.4
15
7. a. 3003-H14 aluminum
b. 2048, plate aluminum
8. a. AZ31B magnesium
b. AM100A casting magnesium
9. a. Ti-5AI-2.5Sn
b. Ti-6Al-4V
10. Aluminum bronze, 9%
(copper alloy)
11. Monel 400 (nickel alloy)
12. AC41A zinc
13. 50:50 solder (lead alloy)
14. Nb-1 Zr (refractory metal)
15. Dental gold alloy (precious
metal)
8-16
8
15
2
15
10
34
179 (26 × 10')
283 (41)
579 (84)
328 (47.6)
42 (6.0)
241 (35)
39.5
33 (4.8)
138 (20)
60
68.9 (10 × 10')
20
310-380
20-35
(45–55)
Transcribed Image Text:Tensile Test Data for Some Typical Metal Alloys Percent Y.S. [MPa (ksi)| E T.S. [MPa (ksi)] elongation at failure Alloy* [GPa (psi)] 1. 1040 carbon steel 2. 8630 low-alloy steel 3. a. 304 stainless steel b. 410 stainless steel 4. L2 tool steel 5. Ferrous superalloy (410) 6. a. Ductile iron, quench b. Ductile iron, 60–40–18 200 (29 × 10) 600 (87) 680 (99) 205 (30) 700 (102) 1,380 (200) 700 (102) 580 (84) 329 (48) 145 (21) 416 (60) 220 (32) 83 (12) 827 (120) 825 (120) 320 (46.4) 750 (109) 800 (116) 515 (75) 800 (116) 1,550 (225) 800 (116) 750 (108) 461 (67) 150 (22) 457 (66) 290 (42) 150 (22) 862 (125) 895 (130) 652 (94.5) 17 22 193 (28 × 10) 200 (29 х 10) 40 22 12 22 200 (29 × 10) 165 (24 x 10) 169 (24.5 × 10) 70 (10.2 × 10°) 70.3 (10.2 × 10) 45 (6.5 x 10) 45 (6.5 × 10°) 107–110 (15.5–16 × 10') 110 (16 x 10) 110 (16.1 × 10) 9.4 15 7. a. 3003-H14 aluminum b. 2048, plate aluminum 8. a. AZ31B magnesium b. AM100A casting magnesium 9. a. Ti-5AI-2.5Sn b. Ti-6Al-4V 10. Aluminum bronze, 9% (copper alloy) 11. Monel 400 (nickel alloy) 12. AC41A zinc 13. 50:50 solder (lead alloy) 14. Nb-1 Zr (refractory metal) 15. Dental gold alloy (precious metal) 8-16 8 15 2 15 10 34 179 (26 × 10') 283 (41) 579 (84) 328 (47.6) 42 (6.0) 241 (35) 39.5 33 (4.8) 138 (20) 60 68.9 (10 × 10') 20 310-380 20-35 (45–55)
A 10-mm-diameter bar of 1040 carbon steel (see Table 6.1) is subjected
to a tensile load of 50,000 N, taking it beyond its yield point. Calculate
the elastic recovery that would occur upon removal of the tensile load.
Transcribed Image Text:A 10-mm-diameter bar of 1040 carbon steel (see Table 6.1) is subjected to a tensile load of 50,000 N, taking it beyond its yield point. Calculate the elastic recovery that would occur upon removal of the tensile load.
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