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commercial alloys

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Published: 01 November 2007
Fig. 7.13 Corrosion rates of commercial alloys as well as experimental Fe-30Ni-20Cr with various aluminum contents in 100% H 2 S at 593 °C (1100 °F). Note the upper curve shows the corrosion rates as a function of chromium content in the alloy, while the lower curve show the corrosion rates More
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Published: 01 October 2011
Fig. 14.24 Phases present in various commercial alloys at various quenching temperatures. Source: Ref 14.10 More
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Published: 01 January 2015
Fig. 4.11 Phases present in standard commercial alloys at various quenching temperatures More
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Published: 01 October 2012
Fig. 1.3 Aluminum alloys used for commercial aircraft. (a) 2 xxx alloys for fuselage. (b) 7 xxx alloys for wings. Source: Ref 1.1 More
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Published: 01 November 2012
Fig. 25 Comparison of 2 xxx and 7 xxx commercial aluminum alloys. (a) Notch toughness vs. yield strength. (b) Unit propagation energy vs. yield strength. Source: Ref 11 More
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Published: 01 July 1997
Fig. 5 Longitudinal weldment tensile data for commercial titanium alloys. Source: Ref 2 More
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080001
EISBN: 978-1-62708-304-1
... eight basic modes of high-temperature corrosion as well as the effect of external and residual stresses. It also provides an extensive amount of engineering data associated primarily with commercial alloys. high-temperature corrosion METALS AND ALLOYS will react during high-temperature...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.t61170432
EISBN: 978-1-62708-297-6
... Abstract This article examines the composition and properties of magnesium and its alloys. It discusses alloy and temper designations, applications and product forms, and commercial alloy systems, and explains how alloying elements affect physical and mechanical properties, processing...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.t61170107
EISBN: 978-1-62708-297-6
... supporting the carbide phase can be adjusted via alloy content and heat treatment to optimize the balance between abrasion resistance and impact toughness. It also describes the effect of alloying elements and inoculants on various properties and behaviors and provides information on commercial alloy grades...
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Published: 01 May 2018
FIG. 9.10 The Boeing 777 is the first commercial plane to use a titanium alloy (Ti-10V-2Fe-3Al) for landing gear. Source: Wikimedia Commons/Altair78. More
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Published: 01 December 2004
Fig. D2.26 Growth and hardness curves for aluminum alloy 355.0 with various commercial tempers and aging at 350 °F, permanent mold. Zero hour data is as-cast. Data at 0.3 h is after the commercial heat treatment. Data for aging at 350 °F is then given. Specimen: 1.125 diam × 12 in. rod More
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Published: 31 December 2020
approximate those of commercial alloys 2025 and 2219, and the principles apply to the other heat treatable alloys. More
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Published: 01 November 2007
Fig. 3.52 Correlation between weight loss (mg/cm 2 ) and the depth of metal loss (mils) for commercial alloys that are primarily chromia formers tested in air at 980 °C (1800 °F)/720 days, 1095 °C (2000 °F)/360 days, and 1150 °C (2100 °F)/360 days. Alloys tested were 230, 617, 601, 556, HR160 More
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Published: 01 July 2000
Fig. 7.31 Effect of seawater velocity on corrosion mode of a range of commercial alloys. Source: Ref 51 More
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Published: 01 June 1983
Figure 8.10 Fracture toughness vs. strength level for a wide variety of commercial alloys tested at 295 and 4 K. More
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Published: 01 November 2007
Fig. 3.53 Oxidation penetration (metal loss + internal attack) as a function of test temperature for 1 year in air for a variety of commercial alloys. Source: Ref 15 More
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Published: 01 November 2007
Fig. 3.57 Effect of oxygen concentration in the N 2 -O 2 mixture on the oxidation penetration (metal loss + internal attack) after 1 year at 927 °C (1700 °F) for various commercial alloys. 1.0 mils = 0.025 mm. Source: Ref 15 More
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Published: 01 December 2004
Fig. 9 Typical “on-cooling” Gleeble curves of strength and ductility as functions of test temperature for several commercial alloys. Material Alloy type Nominal composition, wt% René 41 Nickel-base superalloy 0.09 C, 19 Cr, 10 Mo, 11 Co, 3 Ti, 1.5 Al, 1.35 Fe, bal Ni Alloy More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120001
EISBN: 978-1-62708-269-3
...) of titanium can be comparable to that of lower-strength martensitic stainless and is better than that of austenitic or ferritic stainless. Alloys can have ultimate strengths comparable to iron-base superalloys, such as A286, or cobalt-base alloys, such as L605. The commercial alloys of titanium are useful...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080409
EISBN: 978-1-62708-304-1
... and increasing nickel in Fe-Ni-Cr alloys. HW alloy (Fe-12Cr-60Ni) was consistently the best performer among the four commercial cast alloys (HW, HT, HK, and HH alloys) studied. These authors further noted that intergranular attack generally followed grain-boundary carbides. Thus, lowering carbon from 0.4...