Materials Science and Engineering Handbook [CRC Press 2001] Episode 8 pps

Table 245. RUPTURE STRENGTH OF REFRACTORY METAL ALLOYS
(SHEET 1 OF 2)
Class Alloy Alloying Additions (%) Form Condition
Temperature
(°F)
10-h rupture
(ksi)
Niobium and
Niobium Alloys
Pure Niobium — All Recrystallized 2000 5.4
Nb–1Zr 1 Zr All Recrystallized 2000 14
SCb291 10 Ta, 10 W Bar, Sheet Recrystallized 2000 9
C129 10 W, 10 Hf, 0.1 Y Sheet Recrystallized 2400 15
FS85 28 Ta, 11 W, 0.8 Zr Sheet Recrystallized 2400 12
SU31 17 W, 3.5 Hf, 0.12 C, 0.03 Si Bar, Sheet Special Thermal Processing 2400 22
Molybdenum and
Molybdenum Alloys
Pure Molybdenum — All Stress-relieved Annealed 1800 25
Low C Mo None All Stress-relieved Annealed 1800 24
TZM 0.5 Ti, 0.08 Zr, 0.015 C All Stress-relieved Annealed 2400 23
TZC 1.0 Ti, 0.14 Zr, 0.02 to 0.08 C All Stress-relieved Annealed 2400 28
Mo–5Re 5 Re All Stress-relieved Annealed 3000 1
Mo–30W 30 W All Stress-relieved Annealed 2000 20
To convert (ksi) to (MPa), multiply by 6.89
Data from ASM Engineering Materials Reference Book, Second Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p106, (1994).
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Tantalum Alloys Unalloyed None All Recrystallized 2400 2.5

TA–10W 10 W All Recrystallized 2400 20
Tungsten Alloys Unalloyed None
Bar, Sheet,
Wire
Stress-relieved Annealed 3000 6.8
W–2 ThO
2
2 ThO
2
Bar, Sheet,
Wire
Stress-relieved Annealed 3000 18
W–3 ThO
2
3 ThO
2
Bar, Wire Stress-relieved Annealed 3000 18
W–4 ThO
2
4 ThO
2
Bar Stress-relieved Annealed 3000 18
W–15 Mo 15 Mo Bar, Wire Stress-relieved Annealed 3000 12
W–50 Mo 50 Mo Bar, Wire Stress-relieved Annealed 3000 12
W–25 Re 25 Re
Bar, Sheet,
Wire
Stress-relieved Annealed 3000 10
Table 245. RUPTURE STRENGTH OF REFRACTORY METAL ALLOYS
(SHEET 2 OF 2)

Class Alloy Alloying Additions (%) Form Condition
Temperature
(°F)
10-h rupture
(ksi)
To convert (ksi) to (MPa), multiply by 6.89
Data from ASM Engineering Materials Reference Book, Second Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p106, (1994).
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Table 246. RUPTURE STRENGTH OF SUPERALLOYS
(SHEET 1 OF 3)
Alloy
*
Temperature (°C)
Stress Rupture
100 h
(MPa)
1000 h
(MPa)
Incoloy 800 650 220 145
760 115 69
870 45 33
Incoloy 801 650 250 —
730 145 —
815 62 —
Incoloy 802 650 240 170
760 145 105

870 97 62
Inconel 600 815 55 39
870 37 24
Inconel 601(a) 540 — 400
870 48 30
980 23 14
Inconel 617(b) 815 140 97
925 62 —
980 41 —
Inconel 625(a) 650 440 370
815 130 93
870 72 48
Inconel 718(c) 540 — 951
595 860 760
650 690 585
Inconel 751(d) 815 200 125
870 120 69
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM
International, Materials Park, OH, p391, (1993).
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Inconel X–750(e) 540 — 827
870 83 45
925 58 21
N–155, bar(f) 650 360 295
730 195 150
870 97 66

N–155(g) 650 380 290
N–155, sheet(f) 980 39 20
Nimonic 75(h) 815 38 24
870 23 15
925 14 10
980 — 7.6
Nimonic 80A(j) 540 — 825
815 185 115
870 105 —
Nimonic 90(j) 815 240 155
870 150 69
925 69 —
Nimonic 105(k) 815 325 225
870 210 135
Nimonic 115(m) 815 425 315
870 315 205
925 205 130
Table 246. RUPTURE STRENGTH OF SUPERALLOYS
(SHEET 2 OF 3)
Alloy
*
Temperature (°C)
Stress Rupture
100 h
(MPa)
1000 h
(MPa)
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM
International, Materials Park, OH, p391, (1993).
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820
*
(a) Solution treat 1150 °C.
(b) Solution treat 1175 °C.
(c) Heat treat to 980 °C plus 720 °C hold for 8 h, furnace cool to 620 °C hold for 8 h.
(d) 730 °C hold for 2h.
(e) Heat treat to 1150 °C plus 840 °C hold for 24h, plus 705 °C hold for 20h.
(f) Solution treated and aged.
(g) Stress-relieved forging.
(h) Heat treat to 1050 °C hold for 1 h.
(j) Heat treat to 1080 °C hold for 8 h, plus 700 °C hold for 16 h.
(k) Heat treat to 1150 °C hold for 4 h, plus 1050 °C hold for 16 h, plus 850 °C hold for 16 h.
(m) Heat treat to 1190 °C hold for 1.5 h, plus 1100 °C hold for 6 h.
(n) Heat treat to 1150 °C hold for 2 h, water quench, plus 800 °C hold for 8 h.
Nimonic 263(n) 815 170 105
870 93 46
925 45 —
Table 246. RUPTURE STRENGTH OF SUPERALLOYS
(SHEET 3 OF 3)
Alloy
*
Temperature (°C)
Stress Rupture
100 h
(MPa)
1000 h
(MPa)

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM
International, Materials Park, OH, p391, (1993).
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821
Table 247. MODULUS OF RUPTURE FOR
S
I
3
N
4
AND AL
2
O
3
COMPOSITES
Matrix
Dispersed
Phase
Modulus of Rupture
(MPa)
RT 1000 °C 1200 °C
Si
3
N
4
+ 6 wt % Y
2

O
3
None 110.9 ± 1.6 88.3 ± 3.5 49.2 ± 5.0
Si
3
N
4
+ 6 wt % Y
2
O
3
TiC 80.6 ± 5.9 120.4 ± 12.2 64.4 ± 2.9
(Ti, W) C 75.5 ± 3.2 86 ± 0 52.9 ± 0.5
WC 89.1 ± 31.8 136.4 ± 1.6 55.7 ± 0.5
TaC 86.2 ± 7.3 124.5 ± 16.0 43.2 ± 2.0
HfC 86 ± 0.8 — 68.6 ± 0.5
SiC 97.6 ± 8.5 94.0 ± 4.9 52.3 ± 3.2
Al
2
O
3
TiC 72.2 ± 13.0 69.4 ± 4.3 57.0 ± 4.1
Containing 30 Vol % of Metal Carbide Dispersoid (2 µm average particle diameter)
Data from ASM Engineering Materials Reference Book, Second Edition, Michael Bauccio,
Ed., ASM International, Materials Park, OH, p169,(1994).
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822

Table 248. POISSON'S RATIO OF
W
ROUGHT TITANIUM ALLOYS
Class Metal or Alloy Poisson's Ratio
Commercially Pure 99.5 Ti 0.34
99.2 Ti 0.34
99.1 Ti 0.34
99.0Ti 0.34
99.2 Ti–0.2Pd 0.34
Near Alpha Alloys Ti-8Al-1Mo-1V 0.32
Ti-5Al-5Sn-2Zr-2Mo-0.25Si 0.326
Alpha-Beta Alloys Ti-6Al-4V 0.342
Ti-6Al-4V (low O
2
)
0.342
Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.25Si 0.327
Beta Alloys Ti-13V-11Cr-3Al 0.304
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM
International, Materials Park, OH, p511, (1993).
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Table 249. POISSON’S RATIO FOR CERAMICS
(SHEET 1 OF 2)
Class Ceramic Poisson’s Ratio
Borides
Titanium Diboride (TiB

2
)
0.09-0.28
(6.0
µm grain size, ρ=4.46g/cm
3
)
0.10
(3.5 µm grain size, ρ=4.37g/cm
3
, 0.8wt% Ni)
0.12
(6.0 µm grain size, ρ=4.56g/cm
3
, 0.16wt% Ni)
0.11
(12.0 µm grain size, ρ=4.66g/cm
3
, 9.6wt% Ni)
0.15
Zirconium Diboride (ZrB
2
)
0.144
Carbides
Boron Carbide (B
4
C)
0.207
Hafnium Monocarbide (HfC) 0.166

Silicon Carbide (SiC)
(
ρ = 3.128 g/cm
3
)
0.183-0.192 at room temp.
Tantalum Monocarbide (TaC) 0.1719 -0.24
Titanium Monocarbide (TiC) 0.187-189
Tungsten Monocarbide (WC) 0.24
Zirconium Monocarbide (ZrC)
(
ρ = 6.118 g/cm
3
)
0.257
Nitrides
Trisilicon tetranitride (Si
3
N
4
)
0.24
(presureless sintered) 0.22-0.27
Oxides
Aluminum Oxide (Al
2
O
3
)
0.21-0.27

Beryllium Oxide (BeO) 0.26-0.34
Cerium Dioxide (CeO
2
)
0.27-0.31
Magnesium Oxide (MgO)
(
ρ = 3.506 g/cm
3
)
0.163 at room temp.
Thorium Dioxide (ThO
2
)
(ρ=9.722 g/cm
3
)
0.275
Source: data compiled by J.S. Park from No. 1 Materials Index, Peter T.B. Shaffer, Plenum Press,
New York, (1964); Smithells Metals Reference Book, Eric A. Brandes, ed., in association with
Fulmer Research Institute Ltd. 6th ed. London, Butterworths, Boston, (1983); and Ceramic
Source, American Ceramic Society (1986-1991)
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824
Oxides
(Con’t)
Titanium Oxide (TiO

2
)
0.28
Uranium Dioxide (UO
2
)
(ρ=10.37 g/cm
3
)
0.302
Zirconium Oxide (ZrO
2
)
0.324-0.337 at room temp.
(partially stabilized) 0.23
(fully stabilized) 0.23-0.32
(plasma sprayed) 0.25
Cordierite (2MgO 2Al
2
O
3
5SiO
2
)
(ρ=2.3g/cm
3
)
0.21
(ρ=2.1g/cm
3

)
0.17
(glass) 0.26
Mullite (3Al
2
O
3
2SiO
2
)
(ρ=2.779 g/cm
3
)
0.238
Spinel (Al
2
O
3
MgO)
(ρ=3.510 g/cm
3
)
0.294
Silicide
Molybdenum Disilicide (MoSi
2
)
0.158-0.172
Table 249. POISSON’S RATIO FOR CERAMICS
(SHEET 2 OF 2)

Class Ceramic Poisson’s Ratio
Source: data compiled by J.S. Park from No. 1 Materials Index, Peter T.B. Shaffer, Plenum Press,
New York, (1964); Smithells Metals Reference Book, Eric A. Brandes, ed., in association with
Fulmer Research Institute Ltd. 6th ed. London, Butterworths, Boston, (1983); and Ceramic
Source, American Ceramic Society (1986-1991)
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825
Table 250. POISSON’S RATIO OF GLASS
(SHEET 1 OF 2)
Class Composition Poisson’s Ratio Temperature
SiO
2
glass
0.166–0.177 room temp.
SiO
2
–Na
2
O glass (15% mol Na
2
O)
0.183 room temp.
(20% mol Na
2
O)
0.203 room temp.
(25% mol Na

2
O)
0.219 room temp.
(30% mol Na
2
O)
0.236 room temp.
(33% mol Na
2
O)
0.249 room temp.
(35% mol Na
2
O)
0.248 room temp.
SiO
2
–PbO glass
(24.6% mol PbO) 0.249
(30.0% mol PbO) 0.174
(35.7% mol PbO) 0.252
(38.4% mol PbO) 0.150
(45.0% mol PbO) 0.219
(50.0% mol PbO) 0.259
(55.0% mol PbO) 0.222
(60.0% mol PbO) 0.281
(65.0% mol PbO) 0.283
B
2
O

3
glass
0.288–0.309 room temp.
Source: data compiled by J.S. Park from O. V. Mazurin, M. V. Streltsina and T. P. Shvaiko–
Shvaikovskaya, Handbook of Glass Data, Part A and Part B, Elsevier, New York, 1983
8.26 Mechanical Page 825 Wednesday, December 31, 1969 17:00
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CRC Handbook of Materials Science & Engineering
826
B
2
O
3
–Na
2
O glass (5.5% mol Na
2
O)
0.279
(10% mol Na
2
O)
0.2740 15˚C
(15.4% mol Na
2
O)
0.271
(20% mol Na
2

O)
0.2860 15˚C
(22.8% mol Na
2
O)
0.272
(25% mol Na
2
O)
0.2713
15˚C

(29.8% mol Na
2
O)
0.274
(33.3% mol Na
2
O)
0.2771 15˚C
(37% mol Na
2
O)
0.2739 15˚C
(37.25% mol Na
2
O)
0.292
Table 251. POISSON'S RATIO OF
S

ILICON CARBIDE SCS–2–AL
Fiber orientation No. of plies Poisson's Ratio
0° 6, 8, 12 0.268
90° 6, 12,40 0.124
± 45° 8, 12, 40 0.395
Data from ASM Engineering Materials Reference Book, Second Edition, Michael Bauccio,
Ed., ASM International, Materials Park, OH, p149,(1994).
Table 250. POISSON’S RATIO OF GLASS
(SHEET 2 OF 2)
Class Composition Poisson’s Ratio Temperature
Source: data compiled by J.S. Park from O. V. Mazurin, M. V. Streltsina and T. P. Shvaiko–
Shvaikovskaya, Handbook of Glass Data, Part A and Part B, Elsevier, New York, 1983
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Table 252. COMPRESSION POISSON’S RATIO OF
T
REATED DUCTILE IRONS
Treatment Compression Poisson’s Ratio
60-40-18 0.26
65-45-12 0.31
80-55-06 0.31
120 90-02 0.27
Source: data from ASM Metals Reference Book, Second Edition, American Society for
Metals, Metals Park, Ohio 44073, p169-170, (1984).
Table 253. TORSION POISSON’S RATIO OF
T
REATED DUCTILE IRONS

Treatment Torsion Poisson’s Ratio
60-40-18 0.29
65-45-12 0.29
80-55-06 0.31
120 90-02 0.28
Source: data from ASM Metals Reference Book, Second Edition, American Society for
Metals, Metals Park, Ohio 44073, p169-170, (1984).
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828
Table 254. ELONGATION OF TOOL STEELS

Type Condition
Elongation
(%)
L2 Annealed 25
Oil quenched from 855 •C and single tempered at:
205 •C 5
315 •C 10
425 •C 12
540 •C 15
650 •C 25
L6 Annealed 25
Oil quenched from 845 •C and single tempered at:
315 •C 4
425 •C 8
540 •C 12
650 •C 20

S1 Annealed 24
Oil quenched from 930 •C and single tempered at:
205 •C
315 •C 4
425 •C 5
540 •C 9
650 •C 12
S5 Annealed 25
Oil quenched from 870 •C and single tempered at:
205 •C 5
315 •C 7
425 •C 9
540 •C 10
650 •C 15
S7 Annealed 25
Fan cooled from 940 •C and single tempered at:
205 •C 7
315 •C 9
425 •C 10
540 •C 10
650 •C 14
Source: Data from ASM Metals Reference Book, Second Edition, American Society for
Metals, Metals Park, Ohio 44073, p241, (1984).
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829
Table 255. ELONGATION OF DUCTILE IRONS

Specification Number Grade or Class
Elongation
(%)
ASTM A395-76
ASME SA395 60-40-18 18
ASTM A476-70(d);
SAE AMS5316 80-60-03 3
ASTM A536-72,
MIL-1-11466B(MR) 60-40-18 18
65-45-12 12
80-55-06 6
100-70-03 3
120-90-02 2
SAE J434c D4018 18
D4512 12
D5506 6
D7003 3
MlL-I-24137(Ships) Class A 15
Class B 7
Class C 20
Source: data from ASM Metals Reference Book, Second Edition, American Society for
Metals, Metals Park, Ohio 44073, p169, (1984).
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Table 256. ELONGATION OF MALLEABLE IRON CASTINGS

Specification Number Grade or Class

Elongation
(%)
Ferritic
ASTM A47, A338; ANSI G48.1;
FED QQ-I-666c 32510 10
35018 18
ASTM A197 5
Pearlitic and Martensitic
ASTM A220; ANSI C48.2;
MIL-I-11444B 40010 10
45008 8
45006 6
50005 5
60004 4
70003 3
80002 2
90001 1
Automotive
ASTM A602; SAE J158 M3210 10
M4504(a) 4
M5003(a) 3
M5503(b) 3
M7002(b) 2
M8501(b) 1
(a) Air quenched and tempered
(b) Liquid quenched and tempered
Source: data from ASM Metals Reference Book, Second Edition, American Society for
Metals, Metals Park, Ohio 44073, p171, (1984).
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Table 257. ELONGATION OF FERRITIC STAINLESS STEELS
(SHEET 1 OF 2)
Type ASTM Specification Form Condition
Elongation
(%)
Type 405 (UNS S40500) A580 Wire Annealed 20
A580 Annealed, Cold Finished 16
Type 409 (UNS S40900) — Bar Annealed 25(a)
Type 429 (UNS S42900) — Bar Annealed 30(a)
Type 430 (UNS S43000) A276 Bar Annealed, Hot Finished 20
A276 Annealed, Cold Finished 16
Type 430Ti(UNS S43036) — Bar Annealed 30(a)
Type 434 (UNS S43400) — Wire Annealed 33(a)
Type 436 (UNS S43600) — Sheet, Strip Annealed 23(a)
(a) Typical Values
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p368 (1993).
8.27 Mechanical L Page 831 Wednesday, December 31, 1969 17:00
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Type 442 (UNS S44200) — Bar Annealed 20(a)
Type 444 (UNS S44400) A176 Plate, Sheet, Strip Annealed 20
Type 446 (UNS S44600) A276 Bar Annealed, Hot Finished 20
A276 Annealed, Cold Finished 16
Table 257. ELONGATION OF FERRITIC STAINLESS STEELS
(SHEET 2 OF 2)
Type ASTM Specification Form Condition
Elongation
(%)
(a) Typical Values

Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p368 (1993).
8.27 Mechanical L Page 832 Wednesday, December 31, 1969 17:00
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Table 258. ELONGATION OF MARTENSITIC STAINLESS STEELS
(SHEET 1 OF 3)
Type ASTM Specification Form Condition
Elongation
(%)
Type 403 (UNS S40300) A276 Bar Annealed, hot finished 20
A276 Annealed, cold finished 16
A276 Intermediate temper, hot finished 15
A276 Intermediate temper, cold finished 12
A276 Hard temper, hot finished 12
A276 Hard temper, cold finished 12
Type 410 (UNS S41000) A276 Bar Annealed, hot finished 20
A276 Annealed, cold finished 16
A276 Intermediate temper, hot finished 15
A276 Intermediate temper, cold finished 12
A276 Hard temper, hot finished 12
A276 Hard temper, cold finished 12
Type 410S (UNS S41008) A176 Plate, Sheet, Strip Annealed 22
Type 410Cb (UNS S41040) A276 Bar Annealed, hot finished 13
A276 Annealed, cold finished 12
A276 Intermediate temper, hot finished 13
A276 Intermediate temper, cold finished 12
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p369-370 (1993).
8.27 Mechanical L Page 833 Wednesday, December 31, 1969 17:00
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Type 414 (UNS S41400) A276 Bar Intermediate temper, hot finished 15
A276 Intermediate temper, cold finished 15
Type 414L — Bar Annealed 20
Type 420 (UNS S42000) — Bar Tempered 205 °C 8
Type 422 (UNS S42200) A565 Bar
Intermediate and hard tempers
for high-temperature service
13
Type 431 (UNS S43100) — Bar Tempered 260 °C 16
— Tempered 595 °C 19
Type 440A (UNS S44002) — Bar Annealed 20
— Tempered 315 °C 5
Type 440B (UNS S44003) — Bar Annealed 18
— Tempered 315 °C 3
Type 440C (UNS S44004) — Bar Annealed 14
— Tempered 315 °C 2
Table 258. ELONGATION OF MARTENSITIC STAINLESS STEELS
(SHEET 2 OF 3)
Type ASTM Specification Form Condition
Elongation
(%)
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p369-370 (1993).
8.27 Mechanical L Page 834 Wednesday, December 31, 1969 17:00
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Type 501 (UNS S50100) — Bar, Plate Annealed 28
— Tempered 540 °C 15
Type 502 (UNS S50200) — Bar, Plate Annealed 30
Table 258. ELONGATION OF MARTENSITIC STAINLESS STEELS
(SHEET 3 OF 3)

Type ASTM Specification Form Condition
Elongation
(%)
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p369-370 (1993).
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Table 259. ELONGATION OF
P
RECIPITATION-HARDENING AUSTENITIC STAINLESS STEELS
Type Form Condition
Elongation
(%)
PH 13–8 Mo (UNS S13800) Bar, Plate, Sheet, Strip H950 6-10
H1000 6-10
15–5 PH (UNS S15500) and 17–4 PH (UNS S17400) Bar, Plate, Sheet, Stript H900 10(a)
H925 10(a)
H1025 12(a)
H1075 13(a)
H1100 14(a)
H1150 16(a)
H1150M 18(a)
17–7 PH (UNS S17700) Bar RH950 6
TH1050 6
(a) For flat rolled products, value varies with thickness.
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p371 (1993).
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*

Typical values
Table 260. ELONGATION OF HIGH–NITROGEN AUSTENITIC STAINLESS STEELS

Type
ASTM
Specification Form Condition
Elongation
(%)
Type 201 (UNS S20100) A276 Bar Annealed 40
Type 202 (UNS S20200) A276 Bar Annealed 40
Type 205 (UNS S20500) — Plate Annealed
*
58
Type 304N (UNS S30451) A276 Bar Annealed 30
Type 304HN (UNS S30452) — Bar Annealed 30
Type 316N (UNS S31651) A276 Bar Annealed 30
Data from ASM Metals Reference Book, Third Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p367 (1993).
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Table 261. TOTAL ELONGATION OF
C
AST ALUMINUM ALLOYS (SHEET 1 OF 3)
Alloy AA No. Temper
Elongation (in 2 in.)
(%)
201.0 T4 20
T6 7

T7 4.5
206.0, A206.0 T7 11.7
208.0 F 2.5
242.0 T21 1.0
T571 0.5
T77 2.0
T571 1.0
T61 0.5
295.0 T4 8.5
T6 5.0
T62 2.0
296.0 T4 9.0
T6 5.0
T7 4.5
308.0 F 2.0
319.0 F 2.0
T6 2.0
F 2.5
T6 3.0
336.0 T551 0.5
T65 0.5
354.0 T61 6.0
355.0 T51 1.5
T6 3.0
T61 1.0
T7 0.5
Source: data from ASM Metals Reference Book, Second Edition, American Society for
Metals, Metals Park, Ohio 44073, (1984).
8.28 Mechanical Page 838 Wednesday, December 31, 1969 17:00
©2001 CRC Press LLC

Shackelford & Alexander
Mechanical Properties
839
355.0 (Con’t) T71 1.5
T51 2.0
T6 4.0
T62 1.5
T7 2.0
T71 3.0
356.0 T51 2.0
T6 3.5
T7 2.0
T71 3.5
T6 5.0
T7 6.0
357.0, A357.0 T62 8.0
359.0 T61 6.0
T62 5.5
360.0 F 3.0
A360.0 F 5.0
380.0 F 3.0
383.0 F 3.5
384.0, A384.0 F 2.5
390.0 F 1.0
T5 1.0
A390.0 F,T5 <1.0
T6 <1.0
T7 <1.0
F,T5 1.0
T6 <1.0

T7 <1.0
Table 261. TOTAL ELONGATION OF
C
AST ALUMINUM ALLOYS (SHEET 2 OF 3)
Alloy AA No. Temper
Elongation (in 2 in.)
(%)
Source: data from ASM Metals Reference Book, Second Edition, American Society for
Metals, Metals Park, Ohio 44073, (1984).
8.28 Mechanical Page 839 Wednesday, December 31, 1969 17:00
©2001 CRC Press LLC