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). 8.25 Mechanical L Page 816 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC 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). 8.25 Mechanical L Page 817 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Mechanical Properties CRC Handbook of Materials Science & Engineering 818 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). 8.26 Mechanical Page 818 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Shackelford & Alexander Mechanical Properties 819 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). 8.26 Mechanical Page 819 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Mechanical Properties CRC Handbook of Materials Science & Engineering 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). 8.26 Mechanical Page 820 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Shackelford & Alexander Mechanical Properties 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). 8.26 Mechanical Page 821 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Mechanical Properties CRC Handbook of Materials Science & Engineering 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). 8.26 Mechanical Page 822 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Shackelford & Alexander Mechanical Properties 823 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) 8.26 Mechanical Page 823 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Mechanical Properties CRC Handbook of Materials Science & Engineering 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) 8.26 Mechanical Page 824 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC [...]... (1 984 ) ©2001 CRC Press LLC 82 8 CRC Handbook of Materials Science & Engineering 8. 26 Mechanical Page 82 9 Wednesday, December 31, 1969 17:00 Mechanical Properties 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 60-40- 18 65-45-12 18 12 80 -55-06 100-70-03 120-90-02 6 3 2 SAE J434c D40 18 D4512... Fiber orientation No of plies Poisson's Ratio 0° 90° ± 45° 6, 8, 12 6, 12,40 8, 12, 40 0.2 68 0.124 0.395 Data from ASM Engineering Materials Reference Book, Second Edition, Michael Bauccio, Ed., ASM International, Materials Park, OH, p149,(1994) ©2001 CRC Press LLC 82 6 CRC Handbook of Materials Science & Engineering 8. 26 Mechanical Page 82 7 Wednesday, December 31, 1969 17:00 Mechanical Properties Table... 0. 281 0. 283 SiO2 glass SiO2–Na2O glass (15% mol Na2O) (20% mol Na2O) (25% mol Na2O) (30% mol Na2O) (33% mol Na2O) SiO2–PbO glass B2O3 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, 1 983 ©2001 CRC Press LLC Shackelford & Alexander 82 5 8. 26 Mechanical Page 82 6... 443.0 B443.0 F F F F 2.5 3.5 8. 0 10.0 C443.0 514.0 5 18. 0 520.0 F F F T4 9.0 9.0 5.0 8. 0 16 535.0 712.0 713.0 F F T5 T5 13 5.0 3.0 4.0 771.0 85 0.0 T6 T5 9.0 10.0 Source: data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, (1 984 ) ©2001 CRC Press LLC 84 0 CRC Handbook of Materials Science & Engineering 8. 29 Mechanical L Page 84 1 Wednesday, December 31,... T6 F T6 2.0 2.0 2.5 3.0 336.0 T551 T65 T61 0.5 0.5 6.0 T51 T6 T61 T7 1.5 3.0 1.0 0.5 3 08. 0 354.0 355.0 Source: data from ASM Metals Reference Book, Second Edition, American Society for Metals, Metals Park, Ohio 44073, (1 984 ) ©2001 CRC Press LLC 83 8 CRC Handbook of Materials Science & Engineering 8. 28 Mechanical Page 83 9 Wednesday, December 31, 1969 17:00 Mechanical Properties Table 261 TOTAL ELONGATION... A47, A3 38; ANSI G 48. 1; FED QQ-I-666c MALLEABLE IRON CASTINGS Grade or Class Elongation (%) 32510 350 18 10 18 5 40010 450 08 45006 50005 10 8 6 5 60004 70003 80 002 90001 4 3 2 1 M3210 M4504(a) M5003(a) 10 4 3 M5503(b) M7002(b) M8501(b) 3 2 1 ASTM A197 Pearlitic and Martensitic ASTM A220; ANSI C 48. 2; MIL-I-11444B Automotive ASTM A602; SAE J1 58 (a) Air quenched and tempered (b) Liquid quenched and tempered... American Society for Metals, Metals Park, Ohio 44073, p171, (1 984 ) ©2001 CRC Press LLC 83 0 CRC Handbook of Materials Science & Engineering 8. 27 Mechanical L Page 83 1 Wednesday, December 31, 1969 17:00 Table 257 ELONGATION OF FERRITIC (SHEET 1 OF 2) STAINLESS STEELS Type ASTM Specification Form Condition Elongation (%) Type 405 (UNS S40500) A 580 A 580 Wire Annealed Annealed, Cold Finished 20 16 Type 409 (UNS... 53(1.5) 45(3) 48( 1) 48( 3) C17500 Copper-cobalt-beryllium alloy C 182 00, C 184 00, C 185 00 Chromium copper C 187 00 leaded copper C 189 00 99.5 Cu, 2.5 Co, 0.6 Be 99.5 Cu(j) 99.0 Cu, 1.0 Pb 98. 75 Cu, 0.75 Sn, 0.3 Si, 0.20 Mn F, R F, W, R, S, T R R, W 28( 5) 40(5) 45 (8) 48( 14) C19000 Copper-nickel-phosphorus alloy C19100 Copper-nickel-phosphorus-tellurium alloy C19400 98. 7 Cu, 1.1 Ni, 0.25 P 98. 15 Cu, 1.1 Ni,... A357.0 359.0 T62 T61 T62 8. 0 6.0 5.5 360.0 A360.0 380 .0 F F F 3.0 5.0 3.0 383 .0 384 .0, A 384 .0 390.0 F F F T5 3.5 2.5 1.0 1.0 A390.0 F,T5 T6 T7 . Data, Part A and Part B, Elsevier, New York, 1 983 8. 26 Mechanical Page 82 5 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Mechanical Properties CRC Handbook of Materials Science & Engineering 82 6 B 2 O 3 –Na 2 O. 540 — 82 7 87 0 83 45 925 58 21 N–155, bar(f) 650 360 295 730 195 150 87 0 97 66 N–155(g) 650 380 290 N–155, sheet(f) 980 39 20 Nimonic 75(h) 81 5 38 24 87 0 23 15 925 14 10 980 — 7.6 Nimonic 80 A(j). 44073, p169-170, (1 984 ). 8. 26 Mechanical Page 82 7 Wednesday, December 31, 1969 17:00 ©2001 CRC Press LLC Mechanical Properties CRC Handbook of Materials Science & Engineering 82 8 Table 254. ELONGATION