Volume 01 - Properties and Selection Irons, Steels, and High-Performance Alloys Part 7 potx

... etc. I. ASM International. Handbook Committee. II. Title: ASM Handbook. TA459.M43 1990 620.1'6 9 0-1 15 ISBN 0-8 71 7 0-3 7 7- 7 (v.1) SAN 20 4 -7 586 ISBN 0-8 71 7 0-3 8 0 -7 Printed in the United States ... Nickel and Nickel Alloys Beryllium-Copper and Beryllium-Nickel Alloys Cobalt and Cobalt Alloys Magnesium and Magnesium Alloys Tin and...

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... W/(m · K) Shrinkage, % 1 0-2 0 32 0-3 80 4 6-5 5 2-5 5 0-5 2 1. 8-2 .2 2 0-3 0 38 0-4 50 5 5-6 5 2-6 4 8-5 0 2. 0-2 .6 4 0-5 0 45 0-5 00 6 5 -7 3 3-6 3 8-4 2 3. 2-4 .6 Thermal Expansion. For irons ... strength and ultrasonic velocity or resonant frequency for test bars of 30 mm (1.2 in.) diameter. M5003 (c) 5 17 75 3...

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... G10390 1039 0.3 7- 0 .44 0 .7 0-1 .00 0.040 0.050 G10400 1040 0.3 7- 0 .44 0.6 0-0 .90 0.040 0.050 G10420 1042 0.4 0-0 . 47 0.6 0-0 .90 0.040 0.050 G10430 1043 0.4 0-0 . 47 0 .7 0-1 .00 0.040 0.050 ... 0.2 5-0 .60 0.04 0.05 M 10 17 0.1 4-0 .21 0.2 5-0 .60 0.04 0.05 M1020 0.1 7- 0 .24 0.2 5-0 .60 0.04 0.05 M1023 0.1 9-0 ....

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... Microstructure and Properties, Annual Statistical Report, Scr. Metall., Proceedings of the Fifth International Conference on the Strength of Metals and Alloys, Encyclopedia of Materials Science and Engineering, 1989 ... Engineering, 1989 SAE Handbook, Materials, 1989 SAE Handbook, Materials, 1989 SAE Handbook, Materials, 1989 SAE Handbook, Materials, International Metallic Material...

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... -0 .15 -0 .006 -0 .18 -0 .0 07 - 0.20 - 0.008 -0 .20 -0 .008 >15 2-2 03 inclusive > 6-8 inclusive - 0.15 - 0.006 -0 .18 -0 .0 07 -0 .20 -0 .008 - 0.23 - 0.009 -0 .23 -0 .009 >20 3-2 29 ... 1 2 inclusive - 0.05 - 0.002 -0 .08 -0 .003 -0 .10 -0 .004 - 0.13 - 0.005 -0 .13 -0...

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... 0.81 0.032 9.52 0. 375 10 .7 2 0.81 0.032 6.35 0.250 6.8 3 1.22 0.048 15.88 0.625 12.0 4 2.59 0.102 22.22 0. 875 7. 6 5 3. 07 0.121 22.22 0. 875 6.2 6 450 0. 177 22.22 0. 875 4.9 Free length ... resistance at elevated temperature High- temperature alloys Inconel X -7 5 0, AMS 5542 Ni 73 , Cr 15, Fe 6 .75 1030 (150) 215 (31) . . . . . . 30 min 40 0-5 90 (75 0-1 100...

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... 10 5- 130 585 85 17 35 0.20 0.5 0- 0.80 0.60 0.5 0- 0.80 0 .7 0- 1.10 0.4 5- 0.65 (p) , (s) 12A (NT) 48 5- 655 7 0- 95 275 40 20 35 0.20 0.4 0- 0 .70 0.60 0.5 0- 0.90 0.6 0- 1.00 0.9 0- 1.20 ... Low-carbon steel 0.29 0.6 0- 1.35 0.1 5- 0.40 (b) 17 0- 250 2 5- 36 31 0- 415 4 5-6 0 2 3-3 0 As-hot rolled carbon- m...

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... Nickel-Chromium-Molybdenum (87xx) Alloy Steels Figure 79 . SAE/AISI 872 0H UNS H 872 00. Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C ( 170 0 ... ( 170 0 °F) Austenitize: 925 °C ( 170 0 °F) Hardenability Curves for Nickel-Chromium-Molybdenum (47xx) Alloy Steels Figure 40. SAE/AISI 471 8H UNS H 471 80. Heat-treating temperature...

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... Trans. ASM, Vol 62, 1969, p 1016 - 1018 100. D.F. Stein, Reversible Temper Embrittlement, Annu. Rev. Mater. Sci. 1 977 , Vol 7, 1 977 , p 12 3-1 53 101. L.D. Jaffe and D.C. Buffum, Isothermal Temper ... Dec 1969, p 161 9-1 623 61. H.J. Kerr and F. Eberle, Graphitization of Low-Carbon and Low-Carbon-Molybdenum Steels, Trans. 25,000 h at 25 °C (75 °F) and 230 °C...

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... O1 870 1600 76 0 -7 90 140 0-1 450 22 40 18 3-2 12 O2 845 1550 84 5 -7 70 1 37 5-1 425 22 40 18 3-2 12 O6 870 1600 76 5 -7 90 141 0-1 450 11 20 18 3-2 17 O7 900 1650 79 0-8 15 145 0-1 500 22 40 19 2-2 17 Shock-resisting ... 1200 (f) 84 5-9 00 155 0- 1650 5-2 0 B or W 17 5- 425 35 0-8 00 S5 Slowly 76 0 1400 87 0-9 25 160 0- 170 0...

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