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Published: 01 August 1999
Fig. 4.15 (Part 2) (e) Heated 30 min at 850 °C, then cooled in still air (normalized). 140 HV. 3% nital. 100×. (f) Heated 30 min at 850 °C, then cooled in still air (normalized). 140 HV. Picral. 2000×. (g) Heated 30 min at 900 °C, then cooled in still air (normalized). 140 HV. 3% nital. 100 More
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Published: 01 December 1995
Fig. 2-29 Track shoe assembly for 140 yd 3 (107 m 3 ) stripping shovel More
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Published: 01 July 2009
Fig. 8.22 Remaining CP cycles after application of 140 PC cycles using predictions by strain-range partitioning (SRP) and damage accumulation More
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Published: 01 June 1983
Figure 9.4 (a) Martensite plates in Fe–33Ni that formed on cooling to 140 K. (b) Martensite plates in Tishomingo meteorite (Fe–32Ni–1Co). Note large grain size of parent austenite and partitioning effect of large martensite plates, which formed first on meteorite cooling. More
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Published: 01 December 2003
Fig. 7 Polycarbonate creep compliance at 23 °C (73.4 °F) and 60 °C (140 °F) with Arrhenius plot of shift factor. a T , amount of curve shift. Source: Ref 22 More
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Published: 01 December 2003
Fig. 1 Tensile strength of polyurethane aged in methanol at 60 °C (140 °F) as a function of exposure time. Source: Ref 8 More
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Published: 01 August 1999
, then cooled in still air (normalized). 130 HV. 3% nital. 100×. (b) Heated 30 min at 750 °C, then cooled in still air (normalized). 130 HV. Picral. 2000×. (c) Heated 30 min at 800 °C, then cooled in still air (normalized). 140 HV. 3% nital. 100×. (d) Heated 30 min at 800 °C, then cooled in still air More
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Published: 01 December 2003
Fig. 25 Determination of relative thermal index (RTI). Control material rated at 150 °C (300 °F); assigned RTI for candidate material was 140 °C (285 °F). Correlation time of 25,000 h corresponds to a 140 °C (285 °F) RTI for candidate material. More
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Published: 01 August 1999
Fig. 4.7 (Part 2) (e) Annealed 4 h at 650 °C, then cooled at 100 °C/h. 100 HV. 3% nital. 500×. (f) Annealed 4 h at 650 °C, then cooled at 100 °C/h. 100 HV. 1% nital + picral. 2000×. (g) Annealed 4 h at 650 °C, then air cooled. 140 HV. 3% nital. 500×. (h) Annealed 4 h at 650 °C, then air More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140211
EISBN: 978-1-62708-335-5
... ... ... 37 255 18 125 13 500 260 1,000 16 110 13 90 25 ... ... 38 260 20 140 12 10,000 14 95 10 70 32 ... ... 34 235 17 115 11 600 315 1,000 9.0 62 8.0 55 48 ... ... 34 235 14 95 12 10,000 8.0 55 6.0 41 51 ... ... 29 200 11 75 13...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140243
EISBN: 978-1-62708-335-5
... ... ... ... ... ... ... ... ... 21 145 10 21 145 20 140 20 140 18 125 ... ... Source data are in English units; metric values are converted and rounded. 224.0-T7: Creep rupture and creep properties Table D5.2 224.0-T7: Creep rupture and creep properties Temperature Time under stress, h Rupture...
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Published: 01 August 1999
) 0.20C-0.004Si-0.45Mn-0.033S-0.016P (wt%). Rim region. 120 HV. 10 vol% pearlite. Picral. 1000×. (f) 0.26C-0.004Si-0.45Mn-0.051S-0.013P (wt%). Core region. 140 HV. 18 vol% pearlite. Picral. 100×. (g) 0.26C-0.004Si-0.45Mn-0.051S-0.013P (wt%). Core region. 140 HV. 18 vol% pearlite. Picral. 1000×. (h More
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Published: 01 August 1999
) 0.20C-0.004Si-0.45Mn-0.033S-0.016P (wt%). Rim region. 120 HV. 10 vol% pearlite. Picral. 1000×. (f) 0.26C-0.004Si-0.45Mn-0.051S-0.013P (wt%). Core region. 140 HV. 18 vol% pearlite. Picral. 100×. (g) 0.26C-0.004Si-0.45Mn-0.051S-0.013P (wt%). Core region. 140 HV. 18 vol% pearlite. Picral. 1000×. (h More
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Published: 01 August 1999
. 100 HV. 3% nital. 500×. (f) Annealed 4 h at 650 °C, then cooled at 100 °C/h. 100 HV. 1% nital + picral. 2000×. (g) Annealed 4 h at 650 °C, then air cooled. 140 HV. 3% nital. 500×. (h) Annealed 4 h at 650 °C, then air cooled. 140 HV. 1% nital + picral. 2000×. More
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Published: 01 October 2011
Fig. 10.8 White cast iron microstructure after heat treatment, exhibiting a network of massive cementite and tempered martensite. Original magnification: 140× More
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Published: 01 December 1995
Fig. 2-140 Assorted corrosion resisting steel castings for gas turbine applications. Weights 25 to 400 lb (11 to 181 kg) More
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Published: 01 December 2015
Fig. 39 Depletion of carbon in pearlite colonies and formation of grain-boundary fissures due to high-temperature hydrogen attack of carbon steel. 140× More
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Published: 01 January 1998
Fig. 5-34 Retardation of martensite transformation as a function of holding time at 60 °C (140 °F) in a 1.1 C-0.2Si-0.3Mn steel. Source: Ref 53 More
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Published: 01 December 2006
Fig. 2 Average EIS calculated corrosion rate during the period of 5–10 days; tests conducted in low chloride solution at 60 °C (140 °F) Source: Ref 7 More
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Published: 01 April 2004
Fig. 3.14 Oxide thickness versus oxidation time for a range of solders held in air 140 °C (284 °F) above their melting point. Adapted from Dong, Schwarz, and Roth [1977 ] More