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1015

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Published: 01 January 1987
Fig. 1016 SEM view of the central area of the fracture surface in Fig. 1015 . Although this is a ductile rupture, it contains very deep secondary cracks. The major pores were sites of alloy second-phase particles that are no longer in place. See Fig. 1017 for an enlarged view of the area More
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Published: 01 August 2013
Fig. 4 Nitrogen gradients in 1015 steel as a function of time of nitriding at 565 °C (1050 °F), using the aerated bath process More
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Published: 01 August 2013
Fig. 8 Nitrogen diffusion in AISI 1015 steel More
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Published: 01 June 2016
Fig. 45 Microstructure of Al-5Cu alloy heated for 1 week at 545 °C (1015 °F), cooled rapidly to 25 °C (77 °F), then held 12 h at (a) 400 °C (750 °F) and (b) 300 °C (570 °F). (a) Optical micrograph (OM). (b) Scanning electron micrograph (SEM). Source: Ref 17 More
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Published: 01 August 2013
Fig. 7 Plots of carbon concentration versus carbon penetration for 1015 steels that were carburized at 930 °C (1705 °F) for 1 h with two different Durofer process base salt regenerators More
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Published: 31 October 2011
Fig. 1 Yield strength as a function of temperature for 1015 steel. Data taken from Ref 18 More
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Published: 01 December 1998
Fig. 16 Nitrogen gradients in 1015 steel as a function of time of nitriding at 565 °C (1050 °F), using the aerated bath process More
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Published: 30 September 2014
Fig. 100 Effect of carburizing time on depth of oxidized zones at different carburizing temperatures for SAE 1015. Source: Ref 43 More
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Published: 01 January 2002
Fig. 70 Depth of oxidized zones as a function of carburizing time at different carburizing temperatures for SAE 1015. Source: Ref 30 More
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Published: 01 June 2016
Fig. 25 Grain size of annealed Ti-5Al-2.5Sn. Annealing temperature has a strong influence on grain size. At the β-transus temperature (1015 °C, or 1860 °F) and higher, grain growth is very rapid. More
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Published: 01 January 1987
Fig. 1015 Surface of a tension-overload fracture in an unnotched specimen of aluminum alloy 7075-T6 having a tensile strength of 520 MPa (75 ksi), with 22% reduction of area. Surface is coarsely fibrous; shear lip has formed two opposing lobes. See also Fig. 1016 and 1017 . 9× More
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Published: 01 January 1987
Fig. 1018 Tension-overload fracture in notched specimen of aluminum alloy 7075-T6. Notched tensile strength, 750 MPa (109 ksi); unnotched tensile strength, same as in Fig. 1015 . Surface is flat and coarsely fibrous. Considerable secondary cracking is evident, even at this low magnification More
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Published: 01 January 1987
Fig. 1021 Cone-shaped fracture surface produced by low-cycle fatigue in aluminum alloy 7075-T6 (same mechanical properties as in Fig. 1015 ). Loading was tension-tension with R = 0.1 and a maximum loading of 310 MPa (45 ksi). Fracture occurred at 26,000 cycles. See also Fig. 1022 More
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Published: 01 January 1987
Fig. 1024 High-cycle fatigue fracture in aluminum alloy 7075-T6 (same mechanical properties as in Fig. 1015 ) loaded in tension-tension with R = 0.1 and a maximum loading of about 159 MPa (23 ksi). Fracture was at 548,000× cycles. Gouge near center is post-test mechanical damage. See also More
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Published: 01 January 1987
Fig. 75 Effect of test temperature on the fracture of Haynes 556, which was tensile tested at a strain rate of 1 s −1 at increasing temperature. (a) Dimple rupture fracture at 1015 °C (1860 °F). At the bottom of many of the dimples are TaC inclusions, which initiated microvoid coalescence. (b More
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Published: 01 January 1993
Fig. 4 Heat-exchanger assembly in brazing fixture and detail of joints brazed with gold brazing filler metal Furnace brazing in dry hydrogen Furnace Bell (a) Fixtures (See illustration) Brazing temperature, °C (°F) 1015 (1860) Hydrogen dew point (max), °C (°F) −60 More
Series: ASM Handbook
Volume: 4D
Publisher: ASM International
Published: 01 October 2014
DOI: 10.31399/asm.hb.v04d.a0006000
EISBN: 978-1-62708-168-9
... E52100 Z 12 C 13 410 22 NCD 2 8620 CC 20 1020 Z 12 C 13 M 403 22 NCD 2 8620H CC 35 1035 Z 12 CN 17.08 301 25 CD 4 (S) 4130 CC 55 1060 Z 12 CNS 25.20 310 25 CD 4 (S) 4130H XC 10 1010 Z 12 CNS 25.20 314 32 C 4 5130H XC 15 1015 Z 15 CN 16.02 431 32 C 4 5132 XC...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006691
EISBN: 978-1-62708-210-5
... 1010–1190 4004 (BAlSi-7) 9.8 … … 1.5 … … … … … … 4008 7 … … 0.38 … 0.9 … … … … 4009 (b) 5.0 1.25 … 0.50 … … bal … 546–621 1015–1150 4010 (c) 7.0 … … 0.35 … … bal … 557–613 1035–1135 4011 (d) 7.0 … … 0.58 … 0.12 bal 0.55 Be 557–613 1035...
Series: ASM Handbook
Volume: 4D
Publisher: ASM International
Published: 01 October 2014
DOI: 10.31399/asm.hb.v04d.a0006002
EISBN: 978-1-62708-168-9
... 11.6 12.5 13.0 13.6 14.2 14.6 15.0 1010 Annealed 12.2 (b) 13.0 (b) 13.5 (b) 13.9 (b) 14.3 (b) 14.7 (b) 15.0 (b) 1010 Unknown 11.9 (c) 12.6 13.3 13.8 14.3 14.7 14.9 1010 Unknown … … … 15.1 (d) … … … 1015 Rolled 11.9 (b) 12.5 (b) 13.0 (b) 13.6 (b...
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.a0001010
EISBN: 978-1-62708-161-0
...-1112) 15.0(b) 15.0 1008 Annealed 12.6(b) 13.1(b) 13.5(b) 13.8(b) 14.2(b) 14.6(b) 15.0(b) 1008 Annealed 11.6 12.5 13.0 13.6 14.2 14.6 14.9 1010 Annealed 12.2(b) 13.0(b) 13.5(b) 13.9(b) 14.3(b) 14.7(b) 1010 Unknown 11.9(c) 12.6 13.3 13.8 14.3 14.7 14.8 1010 Unknown 12.5(b) 15.1(d) 14.2(b) 14.9(b) 1015...