Volume 01 - Properties and Selection Irons, Steels, and High-Performance Alloys Part 2 pptx

... Nickel and Nickel Alloys Beryllium-Copper and Beryllium-Nickel Alloys Cobalt and Cobalt Alloys Magnesium and Magnesium Alloys Tin and Tin Alloys Zinc and Zinc Alloys Lead and Lead Alloys ... of Carbon and Low-Alloy Steels 6 140 21 9 22 567 Specialty Steels and Heat-Resistant Alloys 11 25 2 24 9 163 358 Special Engineering Topics 2 27 29 11...

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... 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 of similar ... (29 .27 ) 47.31 (27 .33) 43. 12 (24 .91) 38.94 (22 .49) 3.9 38.10 (22 .01) 41.0 (23 .69) 39.40 (22 .76) 37.30 (21 .55)...

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... 1.1 0-1 .40 0.040 0.050 G1 522 0 1 522 0.1 8-0 .24 1.1 0-1 .40 0.040 0.050 G1 524 0 1 524 0.1 9-0 .25 1.3 5-1 .65 0.040 0.050 G1 526 0 1 526 0 .2 2- 0 .29 1.1 0-1 .40 0.040 0.050 G1 527 0 1 527 0 .2 2- 0 .29 ... 0.050 G1 023 0 1 023 0 .2 0-0 .25 0.3 0-0 .60 0.040 0.050 G1 025 0 1 025 0 .2 2- 0 .28 0.3 0-0 .60 0.040 0.050 G1 026 0 1 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 .007 -0 .20 -0 .008 - 0 .23 - 0.009 -0 .23 -0 .009 > ;20 3 -2 29 inclusive > 8-9 inclusive - 0.18 - 0.007 -0 .20 -0 .008 -0 .23 -0 .009 - 0 .25 - 0 .010 -0 .25 -0 .010 ... 5147 21 7 20 7 5150 21 2 20 1 5155 22 9 21 7 5160 23 5 22 3 51B60 23 5 22 3 6118 163 156 6150...

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... 22 8 A 22 7 A 22 7 A 22 7 A 22 7 A 22 9 550 80 A 22 8 A 22 7 A 22 7 A 22 7 (~) , A 22 9 A 22 9 A 401 690 100 A 22 8 A 22 9 A 22 9 (f) , A 22 8 A 22 8 (y) , A 401 A 401 (n) . . . 825 120 A 22 8 A 22 8 A 22 8 (}) ... A 22 8 A 22 7 A 22 7 A 22 7 A 22 7 (h) , A 22 9 A 22 9 690 100 A 22 8 A 22 7 A 22 7 (z) , A 22 9 A 401 A 401 (n) . . . 825 120 A...

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... 2 in.), % Low-carbon steel 0 .29 0.6 0- 1.35 0.1 5- 0.40 (b) 17 0- 25 0 2 5- 36 31 0- 415 4 5-6 0 2 3-3 0 As-hot rolled carbon- manganese steel 0.40 1.0 0- 1.65 0.1 5- 0.40 . . . 25 0- 400 3 6- 58 ... 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...

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... Nickel-Chromium-Molybdenum (88xx) Alloy Steels Figure 81. SAE/AISI 8 822 H UNS H8 822 0. Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C ... Nickel-Chromium-Molybdenum (87xx) Alloy Steels Figure 79. SAE/AISI 8 720 H UNS H8 720 0. Heat-treating temperatures recommended by SAE Normalize (for forged or rolled specimens only): 925 °C ....

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... 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 23 0 °C (450 °F). Room-temperature aging ... Embrittlement of Cr-Mo- V Steels, Metall. Trans. A, Vol 6A, Dec 1975, p 22 8 9 -2 29 7 107. D.L. Newhouse et al., Temper Embrittlement Study of Nickel-Chromium-Molybdenum...

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... 87 0-9 00 160 0-1 650 22 40 21 7 -2 55 T2 Do not normalize 87 0-9 00 160 0-1 650 22 40 22 3 -2 55 T4 Do not normalize 87 0-9 00 160 0-1 650 22 40 22 9 -2 69 T5 Do not normalize 87 0-9 00 160 0-1 650 22 40 23 5 -2 77 ... 1600 76 0-7 90 140 0-1 450 22 40 18 3 -2 12 O2 845 1550 84 5-7 70 137 5-1 425 22 40 18 3 -2 12 O6 870 1600 76 5-7 90 141 0-...

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