Subpart PHYSICAL PROPERTIES TABLES COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TE-1 2001 SECTION II TABLE TE-1 THERMAL EXPANSION FOR FERROUS MATERIALS Coefficients for Carbon and Low Alloy Steels (Group 1) [Note (1)] Coefficients for Other Low Alloy Steels (Group 2) [Note (2)] Coefficients for 5Cr–1Mo and 29Cr–7Ni–2Mo–N Steels Temperature, °F A B C A B C A B C 70 100 150 200 250 6.4 6.5 6.7 6.9 7.1 6.4 6.5 6.6 6.7 6.8 0.2 0.6 1.0 1.5 7.0 7.1 7.3 7.5 7.6 7.0 7.1 7.2 7.3 7.3 0.3 0.7 1.1 1.6 6.5 6.6 6.7 6.8 6.9 6.4 6.5 6.6 6.7 6.8 0.3 0.7 1.1 1.5 300 350 400 450 500 7.3 7.5 7.7 7.8 8.0 6.9 7.0 7.1 7.2 7.3 1.9 2.4 2.8 3.3 3.7 7.7 7.9 8.0 8.1 8.3 7.4 7.5 7.6 7.6 7.7 2.1 2.5 3.0 3.5 4.0 7.0 7.2 7.3 7.4 7.4 6.9 6.9 7.0 7.0 7.1 1.9 2.3 2.8 3.2 3.6 550 600 650 700 750 8.2 8.4 8.5 8.6 8.8 7.3 7.4 7.5 7.6 7.7 4.2 4.7 5.2 5.7 6.3 8.4 8.5 8.6 8.6 8.7 7.8 7.8 7.9 7.9 8.0 4.5 5.0 5.5 6.0 6.5 7.5 7.6 7.7 7.8 7.9 7.1 7.2 7.2 7.2 7.3 4.1 4.6 5.0 5.5 5.9 800 850 900 950 1000 8.9 9.0 9.1 9.2 9.3 7.8 7.9 7.9 8.0 8.1 6.8 7.3 7.9 8.4 9.0 8.8 8.8 8.9 9.0 9.0 8.1 8.1 8.1 8.2 8.2 7.1 7.6 8.1 8.7 9.2 8.0 8.0 8.1 8.2 8.2 7.3 7.4 7.4 7.4 7.5 6.4 6.9 7.4 7.9 8.4 1050 1100 1150 1200 1250 9.4 9.5 9.5 9.6 9.6 8.1 8.2 8.3 8.3 8.4 9.6 10.1 10.7 11.3 11.8 9.0 9.1 9.1 9.1 9.1 8.3 8.3 8.3 8.4 8.4 9.7 10.3 10.8 11.4 11.9 8.3 8.3 8.4 8.5 8.5 7.5 7.6 7.6 7.6 7.7 8.9 9.4 9.9 10.4 10.9 1300 1350 1400 1450 1500 9.6 8.4 12.4 9.1 9.1 9.1 9.1 9.1 8.4 8.5 8.5 8.5 8.5 12.4 13.0 13.5 14.1 14.6 8.5 8.6 8.6 7.7 7.7 7.8 11.4 11.9 12.4 648 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services PART D — PROPERTIES Table TE-1 TABLE TE-1 (CONT’D) THERMAL EXPANSION FOR FERROUS MATERIALS Coefficients for 9Cr–1Mo Steels Coefficients for 5Ni–1/4Mo Steels Coefficients for 8Ni and 9Ni Steels Temperature, °F A B C A B C A B C 70 100 150 200 250 5.8 5.9 6.0 6.2 6.3 5.8 5.9 5.9 6.0 6.1 0.2 0.6 0.9 1.3 6.2 6.3 6.6 6.7 6.9 6.2 6.3 6.4 6.5 6.6 0.2 0.6 1.0 1.4 5.5 5.7 6.0 6.3 6.5 5.5 5.6 5.8 5.9 6.1 0.2 0.6 0.9 1.3 300 350 400 450 500 6.4 6.5 6.6 6.8 6.9 6.2 6.2 6.3 6.3 6.4 1.7 2.1 2.5 2.9 3.3 7.1 7.2 7.4 7.5 7.6 6.7 6.8 6.8 6.9 7.0 1.8 2.3 2.7 3.2 3.6 6.6 6.8 6.9 7.0 7.2 6.2 6.3 6.4 6.5 6.6 1.7 2.1 2.5 3.0 3.4 550 600 650 700 750 7.0 7.1 7.2 7.3 7.4 6.5 6.5 6.6 6.6 6.7 3.7 4.1 4.6 5.0 5.4 7.8 7.9 8.0 8.1 8.2 7.1 7.1 7.2 7.3 7.3 4.1 4.5 5.0 5.5 6.0 7.3 7.4 7.5 7.5 7.6 6.6 6.7 6.7 6.8 6.8 3.8 4.3 4.7 5.1 5.6 800 850 900 950 1000 7.4 7.5 7.6 7.7 7.8 6.7 6.8 6.8 6.9 6.9 5.9 6.3 6.8 7.3 7.7 8.3 8.4 8.5 8.6 8.7 7.4 7.5 7.5 7.6 7.6 6.5 7.0 7.5 8.0 8.5 7.6 7.7 7.7 7.8 7.8 6.9 6.9 7.0 7.0 7.0 6.0 6.5 6.9 7.4 7.8 1050 1100 1150 1200 1250 7.8 7.9 8.0 8.0 8.1 7.0 7.0 7.1 7.1 7.1 8.2 8.7 9.1 9.6 10.1 8.8 8.8 8.9 9.0 7.7 7.8 7.8 7.9 9.1 9.6 10.1 10.7 1300 1350 1400 1450 1500 8.1 7.2 10.6 649 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TE-1 2001 SECTION II TABLE TE-1 (CONT’D) THERMAL EXPANSION FOR FERROUS MATERIALS Coefficients for 12Cr, 12Cr–1Al, 13Cr, and 13Cr–4Ni Steels Coefficients for 15Cr and 17Cr Steels Coefficients for 27Cr Steels Temperature, °F A B C A B C A B C 70 100 150 200 250 5.9 6.0 6.2 6.3 6.4 5.9 6.0 6.1 6.2 6.2 0.2 0.6 1.0 1.4 5.3 5.4 5.5 5.7 5.8 5.3 5.4 5.5 5.5 5.6 0.2 0.5 0.9 1.2 5.0 5.1 5.1 5.2 5.3 5.0 5.1 5.1 5.2 5.2 0.2 0.5 0.8 1.1 300 350 400 450 500 6.5 6.6 6.7 6.7 6.8 6.3 6.4 6.4 6.4 6.5 1.7 2.1 2.5 2.9 3.3 5.9 6.0 6.1 6.2 6.3 5.7 5.7 5.8 5.8 5.9 1.6 1.9 2.3 2.7 3.0 5.4 5.4 5.5 5.6 5.7 5.2 5.3 5.3 5.3 5.4 1.4 1.8 2.1 2.4 2.8 550 600 650 700 750 6.8 6.9 6.9 7.0 7.1 6.5 6.5 6.6 6.6 6.6 3.8 4.2 4.6 5.0 5.4 6.4 6.5 6.5 6.6 6.7 5.9 6.0 6.0 6.1 6.1 3.4 3.8 4.2 4.6 5.0 5.7 5.8 5.9 5.9 6.0 5.4 5.4 5.5 5.5 5.5 3.1 3.5 3.8 4.2 4.5 800 850 900 950 1000 7.1 7.2 7.2 7.3 7.3 6.7 6.7 6.7 6.8 6.8 5.8 6.3 6.7 7.1 7.6 6.8 6.8 6.9 7.0 7.0 6.1 6.2 6.2 6.3 6.3 5.3 5.8 6.2 6.6 7.0 6.1 6.2 6.2 6.3 6.4 5.6 5.6 5.7 5.7 5.7 4.9 5.3 5.6 6.0 6.4 1050 1100 1150 1200 1250 7.3 7.4 7.4 7.4 7.5 6.8 6.8 6.9 6.9 6.9 8.0 8.4 8.9 9.3 9.8 7.1 7.1 7.2 7.2 7.2 6.3 6.4 6.4 6.4 6.5 7.5 7.9 8.3 8.7 9.2 6.4 6.5 6.6 6.7 6.7 5.8 5.8 5.8 5.9 5.9 6.8 7.2 7.6 7.9 8.3 1300 1350 1400 1450 1500 7.5 7.5 7.6 7.6 7.6 6.9 7.0 7.0 7.0 7.0 10.2 10.7 11.1 11.6 12.0 7.3 7.3 7.3 7.3 7.4 6.5 6.5 6.6 6.6 6.6 9.6 10.0 10.5 10.9 11.4 6.8 6.9 6.9 7.0 7.1 5.9 6.0 6.0 6.0 6.1 8.8 9.2 9.6 10.0 10.4 650 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services PART D — PROPERTIES Table TE-1 TABLE TE-1 (CONT’D) THERMAL EXPANSION FOR FERROUS MATERIALS Coefficients for Other Austenitic Stainless Steels (Group 4) [Note (4)] Coefficients for Austenitic Stainless Steels (Group 3) [Note (3)] Coefficients for Ductile Cast Iron Temperature, °F A B C A B C A B C 70 100 150 200 250 8.5 8.7 9.0 9.3 9.6 8.5 8.6 8.8 8.9 9.1 0.3 0.8 1.4 2.0 8.7 8.8 8.9 9.0 9.1 8.2 8.2 8.4 8.5 8.6 0.3 0.8 1.3 1.8 5.7 5.8 5.9 6.0 6.1 0.2 0.6 0.9 1.3 300 350 400 450 500 9.8 10.0 10.2 10.3 10.4 9.2 9.3 9.5 9.6 9.7 2.5 3.2 3.7 4.3 5.0 9.1 9.2 9.2 9.2 9.3 8.8 8.8 8.9 9.0 9.1 2.4 3.0 3.5 4.1 4.7 6.3 6.4 6.5 6.7 6.9 1.7 2.1 2.6 3.0 3.5 550 600 650 700 750 10.6 10.7 10.8 10.9 11.0 9.8 9.8 9.9 10.0 10.0 5.6 6.3 6.9 7.6 8.2 9.3 9.4 9.4 9.4 9.5 9.1 9.2 9.2 9.3 9.3 5.3 5.8 6.4 7.0 7.6 6.9 7.0 7.0 7.1 7.2 4.0 4.4 4.9 5.4 5.9 800 850 900 950 1000 11.1 11.1 11.2 11.3 11.4 10.1 10.1 10.2 10.3 10.3 8.8 9.5 10.2 10.8 11.5 9.5 9.6 9.6 9.7 9.7 9.4 9.4 9.5 9.6 9.6 8.2 8.8 9.5 10.1 10.7 7.3 7.3 7.4 7.4 7.5 6.4 6.9 7.4 7.9 8.4 1050 1100 1150 1200 1250 11.5 11.6 11.6 11.7 11.8 10.4 10.5 10.5 10.6 10.6 12.2 12.9 13.6 14.3 15.0 9.8 9.8 9.9 9.9 9.9 9.7 9.7 9.8 9.8 9.9 11.4 12.0 12.7 13.3 14.0 1300 1350 1400 1450 1500 11.9 11.9 12.0 12.1 12.1 10.7 10.7 10.8 10.8 10.8 15.7 16.4 17.2 17.9 18.6 10.0 10.0 10.1 10.2 10.2 9.9 10.0 10.1 10.1 10.2 14.7 15.3 16.0 16.7 17.5 651 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TE-1 2001 SECTION II TABLE TE-1 (CONT’D) THERMAL EXPANSION FOR FERROUS MATERIALS Coefficients for Precipitation Hardened 17Cr–4Ni–4Cu Stainless Steels [Note (5)] Temperature, °F A B C 70 100 150 200 250 5.9 5.9 5.9 5.9 5.9 5.9 5.9 5.9 5.9 5.9 0.2 0.6 0.9 1.3 300 350 400 450 500 5.9 5.9 5.9 5.9 5.9 5.9 5.9 5.9 5.9 5.9 1.6 2.0 2.3 2.7 3.1 550 600 650 700 750 800 5.9 6.0 6.0 6.0 6.1 6.1 5.9 5.9 5.9 5.9 6.0 6.0 3.4 3.8 4.1 4.5 4.9 5.2 Notes appear on following page 652 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services PART D — PROPERTIES Table TE-1 NOTES TO TABLE TE-1 GENERAL NOTES: (a) Coefficient A is the instantaneous coefficient of thermal expansion × 10−6 (in./in./°F) Coefficient B is the mean coefficient of thermal expansion × 10−6 (in./in./°F) in going from 70°F to indicated temperature Coefficient C is the linear thermal expansion (in./100 ft) in going from 70°F to indicated temperature (b) For SI units, multiply coefficients A and B by 1.8 to convert to mm/mm/°C and divide coefficient C by 2.16 to convert to mm/(mW°C) (c) See Table SI-1 for the conversion of temperatures to degrees Celsius NOTES: (1) Group alloys (by nominal composition): Carbon steels (C, C–Mn, C–Si, and 11⁄4Cr–1⁄2Mo–Si ⁄4Ni–1Mo–3⁄4Cr 1Ni–1⁄2Cr–1⁄2Mo C–Mn–Si) ⁄4Cr– ⁄2Mo–Cu C–1⁄4Mo 13⁄4Cr–1⁄2Mo–Ti 11⁄4Ni–1Cr–1⁄2Mo 1 C– ⁄2Mo 2Cr– ⁄2Mo 13⁄4Ni–3⁄4Cr–1⁄4Mo ⁄2Cr–1⁄5Mo–V 21⁄4Cr–1Mo 2Ni–3⁄4Cr–1⁄4Mo 1 ⁄2Cr– ⁄4Mo–Si 3Cr–1Mo 2Ni–3⁄4Cr–1⁄3Mo 1 ⁄2Cr–1⁄2Mo ⁄2Ni–1⁄2Cr–1⁄4Mo 2Ni–11⁄2Cr–1⁄4Mo–V 1 1 ⁄4Cr– ⁄2Ni–Cu ⁄2Ni– ⁄2Cr– ⁄4Mo–V 21⁄2Ni ⁄4Cr–3⁄4Ni–Cu–Al ⁄2Ni–1⁄2Mo–V 23⁄4Ni–11⁄2Cr–1⁄2Mo–V ⁄4Ni–1⁄2Cr–1⁄2Mo–V 31⁄2Ni 1Cr–1⁄5Mo 1Cr–1⁄5Mo–Si ⁄4Ni–1⁄2Cu–Mo 31⁄2Ni–13⁄4Cr–1⁄2Mo–V 1Cr–1⁄2Mo ⁄4Ni–1⁄2Mo–1⁄3Cr–V 4Ni–11⁄2Cr–1⁄2Mo–V ⁄4Ni–1⁄2Mo–Cr–V 1Cr–1⁄2Mo–V 11⁄4Cr–1⁄2Mo (2) Group alloys (by nominal composition): Mn–1⁄4Mo Mn–1⁄2Mo–3⁄4Ni 22Cr–5Ni–3Mo–N Mn–1⁄2Mo Mn–V 23Cr–4Ni–Mo–Cu Mn–1⁄2Mo–1⁄4Ni 18Cr–5Ni–3Mo–N 25Cr–7Ni–4Mo–N Mn–1⁄2Mo–1⁄2Ni (3) Group alloys (by nominal composition): 16Cr–12Ni–2Mo 18Cr–8Ni–N 18Cr–13Ni–3Mo 16Cr–12Ni–2Mo–N 18Cr–10Ni–Cb 18Cr–18Ni–2Si 16Cr–12Ni–2Mo–Ti 18Cr–10Ni–Ti 19Cr–9Ni–Mo–W 18Cr–8Ni 18Cr–11Ni 21Cr–11Ni–N (4) Group alloys (by nominal composition): 29Ni–20Cr–3Cu–2Mo 23Cr–12Ni 25Cr–20Ni–2Mo 20Cr–18Ni–6Mo 25Cr–12Ni 31Ni–31Fe–29Cr–Mo 22Cr–13Ni–5Mn 25Cr–20Ni 44Fe–25Ni–21Cr–Mo (5) These thermal expansion values are representative of solution annealed material Subsequent precipitation hardening treatments may affect thermal expansion behavior 653 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TE-2 2001 SECTION II TABLE TE-2 THERMAL EXPANSION FOR ALUMINUM ALLOYS Coefficients for Aluminum Alloys Temperature, °F A B C 70 100 150 200 12.1 12.5 12.9 13.3 12.1 12.4 12.7 13.0 0.5 1.2 2.0 250 300 350 400 13.6 13.9 14.2 14.6 13.1 13.3 13.4 13.6 2.8 3.7 4.5 5.4 450 500 550 600 14.8 14.9 15.2 15.3 13.8 13.9 14.1 14.2 6.3 7.2 8.1 9.0 GENERAL NOTES: (a) Aluminum alloys represented by these thermal expansion coefficients include: A03560 A93003 A95254 A24430 A93004 A95454 A91060 A95052 A95456 A91100 A95083 A95652 A92014 A95086 A96061 A92024 A95154 A96063 (b) Coefficient A is the instantaneous coefficient of thermal expansion × 10−6 (in./in./°F) Coefficient B is the mean coefficient of thermal expansion × 10−6 (in./in./°F) in going from 70°F to indicated temperature Coefficient C is the linear thermal expansion (in./ 100 ft) in going from 70°F to indicated temperature (c) For SI units, multiply coefficients A and B by 1.8 to convert to mm/mm/°C and divide coefficient C by 2.16 to convert to mm/(mW°C) (d) See Table SI-1 for the conversion of temperatures to degrees Celsius 654 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services PART D — PROPERTIES Table TE-3 TABLE TE-3 THERMAL EXPANSION FOR COPPER ALLOYS Coefficients for Copper Alloys, C1XXXX Series Coefficients for Bronze Alloys Temperature, °F A B C A B 70 100 150 200 250 9.3 9.4 9.5 9.6 9.6 0.3 0.9 1.5 2.1 9.6 9.7 9.9 10.0 10.1 0.4 1.0 1.6 2.3 300 350 400 450 500 9.7 9.8 9.8 9.9 9.9 2.7 3.2 3.8 4.5 5.1 10.1 10.2 10.2 10.3 10.3 550 600 650 700 750 800 10.0 10.0 5.6 6.1 10.4 10.4 10.5 10.5 10.6 10.6 C Coefficients for Brass Alloys A B C 9.3 9.4 9.6 9.8 9.9 2.8 3.5 4.1 4.8 5.3 6.0 6.6 7.3 8.0 8.6 9.3 Coefficients for Copper–Nickel (70Cu–30Ni) Coefficients for Copper–Nickel (90Cu–10Ni) A B C A B C 0.4 1.0 1.5 2.2 8.1 8.2 8.4 8.5 8.6 0.3 0.9 1.3 1.9 10.0 10.1 10.2 10.4 10.5 2.8 3.4 4.1 4.7 5.4 8.7 8.8 8.9 9.0 9.1 2.4 3.0 3.5 4.1 4.7 10.6 10.7 10.8 10.9 11.0 11.2 6.1 6.8 7.5 8.3 9.0 9.8 9.1 9.2 9.2 9.2 5.2 5.9 6.4 7.0 9.5 5.5 GENERAL NOTES: (a) Coefficient A is the instantaneous coefficient of thermal expansion × 10−6 (in./in./°F) Coefficient B is the mean coefficient of thermal expansion × 10−6 (in./in./°F) in going from 70°F to indicated temperature Coefficient C is the linear thermal expansion (in./100 ft) in going from 70°F to indicated temperature (b) For SI units, multiply coefficients A and B by 1.8 to convert to mm/mm/°C and divide coefficient C by 2.16 to convert to mm/(mW°C) (c) See Table SI-1 for the conversion of temperatures to degrees Celsius 655 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TE-4 2001 SECTION II TABLE TE-4 THERMAL EXPANSION FOR NICKEL ALLOYS Coefficients for N02200 and N02201 Coefficients for N04400 and N04405 Coefficients for N06002 Temperature, °F A B C A B C A B C 70 100 150 200 250 6.6 6.8 7.1 7.3 7.5 6.6 6.8 7.0 7.2 7.4 0.2 0.7 1.1 1.6 7.7 7.8 8.0 8.2 8.4 7.7 7.8 7.9 8.1 8.2 0.3 0.8 1.3 1.8 7.3 7.4 7.5 7.6 7.7 7.3 7.4 7.4 7.5 7.6 0.3 0.7 1.2 1.6 300 350 400 450 500 7.7 7.8 8.1 8.3 8.4 7.5 7.6 7.7 7.8 7.9 2.1 2.6 3.1 3.6 4.1 8.5 8.7 8.8 8.9 9.0 8.3 8.4 8.5 8.6 8.7 2.3 2.8 3.4 3.9 4.5 7.8 7.9 7.9 8.0 8.1 7.6 7.7 7.7 7.8 7.8 2.1 2.6 3.1 3.5 4.0 550 600 650 700 750 8.6 8.7 8.8 8.9 9.0 8.0 8.1 8.1 8.2 8.2 4.6 5.1 5.6 6.2 6.7 9.1 9.2 9.3 9.3 9.4 8.8 8.8 8.9 8.9 8.9 5.1 5.6 6.2 6.7 7.3 8.2 8.3 8.4 8.6 8.8 7.9 7.9 8.0 8.0 8.1 4.5 5.0 5.6 6.1 6.6 800 850 900 950 1000 9.1 8.3 8.4 8.4 8.5 8.5 7.2 7.8 8.4 8.9 9.5 9.4 8.9 8.9 9.0 9.0 9.1 7.8 8.4 8.9 9.5 10.1 9.1 8.2 8.3 8.4 8.4 8.5 7.2 7.8 8.3 8.9 9.5 1050 1100 1150 1200 1250 8.6 8.6 8.7 8.7 8.8 10.1 10.6 11.2 11.8 12.4 9.1 9.1 9.1 9.2 9.2 10.7 11.3 11.8 12.4 13.0 8.6 8.6 8.7 8.8 8.8 10.1 10.7 11.3 11.9 12.5 1300 1350 1400 1450 1500 8.8 8.9 8.9 13.0 13.6 14.2 9.2 9.2 9.3 9.3 9.3 13.6 14.2 14.8 15.4 16.0 8.9 9.0 9.0 9.1 9.2 13.1 13.8 14.4 15.1 15.7 656 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TCD 2001 SECTION II TABLE TCD (CONT’D) NOMINAL COEFFICIENTS OF THERMAL CONDUCTIVITY (TC) AND THERMAL DIFFUSIVITY (TD) High Nickel Alloys (Cont’d) Ni–Mo N10001 Cr–Ni–Fe–Mo– Cu–Cb N08020 70Ni–16Cr–7Fe– Ti–Al N07750 Ni–Cr–Fe–Mo–Cu N06007 Ni–Mo–Cr–Fe N10003 Temp., °F TC TD TC TD TC TD TC TD TC TD 70 100 150 200 250 6.1 6.2 6.4 6.5 0.115 0.114 0.116 0.116 6.9 7.2 7.5 7.8 0.198 0.207 0.214 0.223 6.9 7.0 7.2 7.4 7.6 0.132 0.132 0.133 0.133 0.133 5.8 6.0 6.2 6.4 6.7 0.116 0.117 0.116 0.115 0.117 6.1 6.6 6.8 0.114 0.121 0.123 300 350 400 450 500 6.7 6.8 7.0 7.2 7.4 0.118 0.117 0.119 0.121 0.122 8.0 8.3 8.6 8.8 9.1 0.229 0.238 0.246 0.254 0.265 7.8 8.0 8.2 8.4 8.6 0.134 0.136 0.140 0.141 0.143 7.0 7.2 7.4 7.7 7.9 0.121 0.123 0.125 0.128 0.130 7.0 7.2 7.4 7.6 7.8 0.125 0.127 0.130 0.131 0.133 550 600 650 700 750 7.5 7.7 8.0 8.2 8.4 0.121 0.124 0.126 0.127 0.129 9.4 9.7 10.0 10.2 10.5 0.270 0.277 0.286 0.293 0.300 8.8 9.1 9.3 9.5 9.8 0.145 0.148 0.151 0.153 0.156 8.2 8.4 8.6 8.9 9.2 0.134 0.136 0.138 0.142 0.146 8.1 8.3 8.5 8.8 9.0 0.137 0.139 0.143 0.147 0.149 800 850 900 950 1000 8.7 9.0 9.3 9.7 10.0 0.132 0.135 0.138 0.143 0.145 10.8 11.0 11.3 11.6 11.9 0.309 10.0 10.2 10.5 10.7 10.9 0.158 0.160 0.162 0.165 0.169 9.4 9.7 9.9 10.2 10.5 0.148 0.151 0.154 0.157 0.160 9.3 9.5 9.8 10.1 10.4 0.153 0.155 0.160 0.163 0.167 1050 1100 1150 1200 1250 10.4 10.7 11.1 0.149 0.153 0.156 10.7 11.0 11.3 11.5 0.162 0.165 0.169 0.171 10.7 11.1 11.4 11.7 12.1 0.161 0.154 0.152 0.158 0.164 1300 1350 1400 1450 1500 12.5 12.9 13.3 13.7 14.2 0.170 666 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services PART D — PROPERTIES Table TCD TABLE TCD (CONT’D) NOMINAL COEFFICIENTS OF THERMAL CONDUCTIVITY (TC) AND THERMAL DIFFUSIVITY (TD) High Nickel Alloys (Cont’d) Ni–Mo–Cr N10276 Ni–Fe–Cr–Si N08330 Titanium Alloys Ni–Mo N10665 Ni–Mo–Cr– Low C N06455 Unalloyed Titanium (Grades 1, 2, 3, 7, 16, and 17) Titanium Grade Temp., °F TC TD TC TD TC TD TC TD TC TD TC TD 70 100 150 200 250 5.9 6.2 6.4 6.7 TBD TBD TBD TBD TBD 7.2 7.2 7.4 7.7 8.0 0.131 0.131 0.135 0.141 TBD 6.8 6.9 7.0 7.2 0.128 0.129 0.130 0.132 5.8 5.9 6.2 6.5 6.8 0.110 0.112 0.114 0.118 0.121 12.68 12.52 12.25 12.00 11.85 0.359 0.352 0.340 0.331 0.322 5.12 5.25 5.46 5.67 5.87 0.145 0.147 0.150 0.152 0.155 300 350 400 450 500 7.0 7.2 7.5 7.8 8.1 TBD TBD TBD TBD TBD 8.2 8.5 8.8 9.1 9.4 TBD TBD TBD TBD TBD 7.3 7.5 7.6 7.8 8.0 0.134 0.135 0.137 0.139 0.141 7.1 7.4 7.7 7.9 8.2 0.124 0.127 0.130 0.133 0.137 11.72 11.60 11.45 11.35 11.29 0.314 0.306 0.300 0.294 0.290 6.06 6.24 6.40 6.55 6.69 0.158 0.160 0.163 0.166 0.168 550 600 650 700 750 8.4 8.7 8.9 9.2 9.5 TBD TBD TBD TBD TBD 9.7 10.0 10.3 10.6 10.9 TBD TBD TBD TBD TBD 8.2 8.4 8.7 8.8 9.1 0.144 0.146 0.149 0.152 0.154 8.5 8.8 9.1 9.3 9.6 0.141 0.145 0.147 0.150 0.154 11.23 11.20 11.17 11.15 11.18 0.286 0.283 0.280 0.278 0.276 6.81 6.91 0.170 0.172 800 850 900 950 1000 9.8 10.1 10.4 10.7 11.0 TBD TBD TBD TBD TBD 11.2 11.5 11.8 12.1 12.4 TBD TBD TBD TBD TBD 9.4 9.6 10.0 10.3 10.7 0.157 0.160 0.164 0.167 0.171 9.9 10.2 10.5 10.8 11.1 0.158 0.162 0.164 0.169 0.172 11.20 11.23 11.30 11.36 11.43 0.275 0.274 0.273 0.272 0.271 1050 1100 1150 1200 1250 11.3 11.5 11.8 12.1 TBD TBD TBD TBD TBD 12.7 13.0 13.2 13.5 13.8 TBD TBD TBD TBD TBD 11.0 11.4 11.8 12.2 0.175 0.179 0.184 0.188 11.5 11.8 12.1 12.5 0.177 0.181 0.185 0.189 11.51 11.58 0.270 0.270 1300 1350 1400 1450 1500 667 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TCD 2001 SECTION II TABLE TCD (CONT’D) NOMINAL COEFFICIENTS OF THERMAL CONDUCTIVITY (TC) AND THERMAL DIFFUSIVITY (TD) Aluminum Alloys A24430 A03560 A91060 A91100 A92014 A92024 Temp., °F TC TD TC TD TC TD TC TD TC TD TC TD 70 100 150 200 94.0 94.9 96.1 97.2 2.64 2.64 2.63 2.63 92.0 92.9 94.2 95.4 2.61 2.61 2.60 2.60 135.2 133.7 131.7 130.1 3.72 3.65 3.54 3.46 133.1 131.8 130.0 128.5 3.67 3.61 3.50 3.42 89.9 90.9 92.3 93.6 2.47 2.48 2.48 2.48 85.8 86.9 88.5 90.0 2.36 2.37 2.38 2.39 250 300 350 400 98.1 99.0 99.7 100.4 2.63 2.62 2.61 2.60 96.4 97.4 98.2 98.9 2.59 2.59 2.59 2.58 128.7 127.5 126.5 125.6 3.38 3.31 3.25 3.19 127.3 126.2 125.3 124.5 3.35 3.28 3.23 3.17 94.7 95.7 96.6 97.4 2.48 2.48 2.47 2.47 91.3 92.4 93.4 94.4 2.39 2.40 2.40 2.39 Aluminum Alloys (Cont’d) A93003 A95052 & A95652 A93004 A95083 A95086 Temp., °F TC TD TC TD TC TD TC TD TC TD 70 100 150 200 102.3 102.8 103.5 104.2 2.81 2.80 2.78 2.76 94.0 94.9 96.1 97.2 2.60 2.60 2.59 2.59 79.6 80.8 82.7 84.4 2.22 2.23 2.25 2.27 67.2 68.7 70.8 72.8 1.88 1.91 1.94 1.97 73.4 74.8 76.8 78.7 2.05 2.08 2.10 2.12 250 300 350 400 104.7 105.2 105.7 106.1 2.75 2.73 2.71 2.69 98.1 99.0 99.7 100.4 2.59 2.58 2.57 2.56 85.9 87.2 88.4 89.6 2.28 2.29 2.30 2.30 74.6 76.2 77.8 79.2 1.99 2.01 2.03 2.05 80.3 81.9 83.2 84.5 2.14 2.16 2.17 2.18 Aluminum Alloys (Cont’d) A95154 & A95254 A95454 A95456 A96061 A96063 Temp., °F TC TD TC TD TC TD TC TD TC TD 70 100 150 200 73.4 74.8 76.8 78.7 2.05 2.08 2.10 2.12 77.5 78.8 80.8 82.5 2.15 2.17 2.19 2.21 67.2 68.7 70.8 72.8 1.89 1.91 1.94 1.97 96.1 96.9 98.0 99.0 2.66 2.66 2.65 2.65 120.8 120.3 119.7 119.1 3.34 3.30 3.23 3.18 250 300 350 400 80.3 81.9 83.2 84.5 2.14 2.16 2.17 2.18 84.1 85.5 86.7 87.9 2.23 2.24 2.25 2.25 74.6 76.3 77.8 79.2 2.00 2.02 2.04 2.05 99.8 100.6 101.3 101.9 2.64 2.63 2.62 2.62 118.3 118.3 117.9 117.6 3.13 3.09 3.04 3.00 668 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services PART D — PROPERTIES Table TCD TABLE TCD (CONT’D) GENERAL NOTES: (a) TC is the thermal conductivity, Btu/hr-ft-°F, and TD is the thermal diffusivity, ft2/hr: TD p TC (Btu/hr-ft-°F) density (lb/ft3) × specific heat (Btu/lb-°F) (b) Values of thermal expansion and thermal diffusivity should be used with the understanding that there is an associated ±10% uncertainty This uncertainty results from compositional variations and variables associated with original data acquisition and analysis (c) For SI units, multiply TC by 1.7295 to convert to W/(mWK) and TD by 2.58064×10-5 to convert to m2/s (d) See Table SI-1 for the conversion of temperatures to degrees Celsius NOTES: (1) Material Group A includes plain carbon steels in which there are no specified amounts of manganese or silicon (2) Material Group B includes carbon steels in which there are specified amounts of manganese and/or silicon, with or without additional small amounts of columbium, titanium, or vanadium (microalloyed steels) Also includes: 3 ⁄4Cr–1⁄2Ni–Cu ⁄4Ni–1⁄2Cu–Mo 1Cr–1⁄2Mo–Si 21⁄2Ni (3) Material Group C includes the following carbon–moly steels: C–1⁄4Mo C–1⁄2Mo The following low chrome steels: ⁄2Cr–1⁄5Mo–V 1Cr–1⁄2Mo 1 ⁄2Cr– ⁄4Mo–Si 11⁄4Cr–1⁄2Mo ⁄2Cr–1⁄2Mo 11⁄4Cr–1⁄2Mo–Si ⁄2Cr–1⁄2Ni–1⁄5Mo 13⁄4Cr–1⁄2Mo–Cu ⁄4Cr–3⁄4Ni–Cu–Al 13⁄4Cr–1⁄2Mo–Ti 1Cr–1Mn–1⁄4Mo 2Cr–1⁄2Mo 1Cr–1⁄5Mo The following manganese steels: Mn–1⁄2Mo Mn–1⁄2Mo–3⁄4Ni Mn–1⁄2Mo–1⁄4Ni Mn–1⁄2Ni–V Mn–1⁄2Mo–1⁄2Ni Mn–V The following nickel steels: ⁄2Ni–1⁄2Cr–1⁄4Mo–V ⁄4Ni–1Mo–3⁄4Cr ⁄2Ni–1⁄2Mo–V 1Ni–1⁄2Cr–1⁄2Mo ⁄4Ni–1⁄2Cr–1⁄2Mo–V 11⁄4Ni–1Cr–1⁄2Mo ⁄4Ni–1⁄2Mo–1⁄3Cr–V 31⁄2Ni–13⁄4Cr–1⁄2Mo–V ⁄4Ni–1⁄2Mo–Cr–V 4Ni–11⁄2Cr–1⁄2Mo-V (4) Material Group D includes the following low chrome steels: 21⁄4Cr–1Mo 3Cr–1Mo The following manganese steel: Mn–1⁄4Mo The following nickel steels: 13⁄4Ni–3⁄4Cr–1⁄4Mo 23⁄4Ni–11⁄2Cr–1⁄2Mo–V 2Ni–3⁄4Cr–1⁄4Mo 5Ni–1⁄4Mo 2Ni–3⁄4Cr–1⁄3Mo 8Ni 2Ni–11⁄2Cr–1⁄4Mo–V 9Ni 2Ni–1Cu (5) Material Group E includes: 5Cr–1⁄2Mo 5Cr–1⁄2Mo–Ti 5Cr–1⁄2Mo–Si TD at 1420°F p 0.105 and at 1425°F p 0.122 ft2/hr (6) Material Group F includes: 9Cr–1Mo TD at 1375°F p 0.109 ft2/hr (7) Material Group G includes: 12Cr 13Cr–4Ni 12Cr–1Al 15Cr 13Cr 17Cr (8) Material Group H includes: 27Cr (9) Material Group I includes: 17Cr–4Ni–4Cu 15Cr–5Ni–3Mo (only to 800°F) 669 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Table TCD 2001 SECTION II TABLE TCD (CONT’D) NOTES (CONT’D): (10) Material Group J includes: 15Cr–6Ni–Cu–Mo (only to 800°F) 17Cr–7Ni–1Al (only to 800°F) 18Cr–8Ni These thermal conductivity and diffusivity values (11) Material Group K includes: 13Cr–8Ni–2Mo (only to 800°F) 29Cr–7Ni–2Mo–N 25Ni–15Cr–2Ti 29Ni–20Cr–3Cu–2Mo 16Cr–12Ni–2Mo 18Cr–5Ni–3Mo 18Cr–10Ni–Cb 18Cr–10Ni–Ti 18Cr–13Ni–3Mo These thermal conductivity and diffusivity values (12) Material Group L includes: 18Cr–18Ni–2Si 22Cr–13Ni–5Mn 24Cr–22Ni–7.5Mo These thermal conductivity and diffusivity values 18Cr–8Ni–S (or Se) 18Cr–11Ni 23Cr–4Ni–Mo–Cu are also appropriate for H, L, N, and LN grades of austenitic stainless steels 19Cr–9Ni–Mo–W 21Cr–11Ni–N 22Cr–5Ni–3Mo–N 23Cr–12Ni 25Cr–7Ni–4Mo–N 25Cr–20Ni 25Cr–20Ni–2Mo 44Fe–25Ni–21Cr–Mo are also appropriate for H, L, N, and LN grades of austenitic stainless steels 25Cr–12Ni 25Cr–35Ni–N–Ce 31Ni–31Fe–29Cr–Mo are also appropriate for H, L, N, and LN grades of austenitic stainless steels 670 COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services −325 31.4 31.2 31.1 29.6 31.6 32.6 33.0 31.2 30.3 31.5 30.5 31.6 30.5 31.6 31.2 Materials Carbon steels with C ≤ 0.30% Carbon steels with C > 0.30% Material Group A [Note (1)] Material Group B [Note (2)] Material Group C [Note (3)] Material Group D [Note (4)] COPYRIGHT American Society of Mechanical Engineers Licensed by Information Handling Services Material Group E [Note (5)] Material Group F [Note (6)] Material Group G [Note (7)] 671 S13800 [Note (8)] S15500 [Note (9)] S45000 [Note (10)] S17400 [Note (11)] S17700 [Note (12)] S66286 [Note (13)] 29.9 31.0 30.7 30.9 29.9 31.0 32.4 30.7 29.7 29.1 31.0 32.0 30.8 30.6 30.5 −200 29.4 30.4 30.1 30.3 29.4 30.4 31.8 30.1 29.1 28.5 30.4 31.4 30.2 30.0 29.9 −100 28.5 29.5 29.2 29.4 28.5 29.5 31.0 29.2 28.3 27.8 29.7 30.6 29.5 29.3 29.2 70 27.8 28.8 28.5 28.7 27.8 28.8 30.2 28.5 27.6 27.1 29.0 29.8 28.8 28.6 28.5 200 27.2 28.2 27.9 28.1 27.2 28.2 29.8 27.9 27.0 26.7 28.5 29.4 28.3 28.1 28.0 300 26.6 27.6 27.3 27.5 26.6 27.6 29.1 27.3 26.5 26.1 27.9 28.8 27.7 27.5 27.4 400 26.1 27.0 26.7 26.9 26.1 27.0 28.7 26.7 25.8 25.7 27.5 28.3 27.3 27.1 27.0 500 25.5 26.4 26.1 26.3 25.5 26.4 28.1 26.1 25.3 25.2 26.9 27.7 26.7 26.5 26.4 600 24.9 25.8 25.6 25.7 24.9 25.8 27.4 25.6 24.8 24.6 26.3 27.1 25.5 25.3 25.3 700 24.2 25.1 24.8 25.0 24.2 25.1 26.8 24.7 24.1 23.9 25.5 26.3 24.2 24.0 23.9 800 23.7 24.5 24.2 24.4 23.7 24.5 26.2 23.2 23.5 23.2 24.8 25.6 22.4 22.3 22.2 900 25.4 21.5 22.8 22.4 23.9 24.6 20.4 20.2 20.1 1000 24.5 19.1 22.1 21.5 23.0 23.7 18.0 17.9 17.8 1100 Modulus of Elasticity E p Value Given × 106 psi, for Temperature, °F, of TABLE TM-1 MODULI OF ELASTICITY E OF FERROUS MATERIALS FOR GIVEN TEMPERATURES 22.0 20.2 19.2 20.5 21.1 1300 20.5 19.2 17.7 18.9 19.4 1400 18.1 1500 Notes appear on following page 23.3 16.6 21.2 20.4 21.8 22.5 15.4 15.3 1200 PART D — PROPERTIES Table TM-1 ... includes: 15Cr–6Ni–Cu–Mo (only to 800°F) 17Cr–7Ni–1Al (only to 800°F) 18Cr–8Ni These thermal conductivity and diffusivity values (11) Material Group K includes: 13Cr–8Ni–2Mo (only to 800°F) 29Cr–7Ni–2Mo–N... compositional variations and variables associated with original data acquisition and analysis (c) For SI units, multiply TC by 1.7295 to convert to W/(mWK) and TD by 2.58064×10-5 to convert to m2/s (d)... thermal expansion (in./100 ft) in going from 70°F to indicated temperature (b) For SI units, multiply coefficients A and B by 1.8 to convert to mm/mm/°C and divide coefficient C by 2.16 to convert