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High-temperature alloys

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Published: 01 July 2009
Fig. 8.2 Comparison of observed creep-fatigue lives of 16 high-temperature alloys with lives calculated by the 10% rule. Source: Ref 8.12 More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.bcp.t52230485
EISBN: 978-1-62708-298-3
...Abstract Abstract This chapter describes the corrosion behavior of beryllium in gaseous atmospheres, including oxygen, nitrogen, carbon dioxide, and carbon monoxide. It also discusses the development of high-temperature corrosion-resistant beryllium alloys. beryllium alloys beryllium...
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Published: 01 June 1983
Figure 4.31 Thermal conductivity of high-temperature nickel alloys. More
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Published: 01 January 2015
Fig. 1.6 Creep behavior of a number of terminal high-temperature titanium alloys and the intermetallic compounds Ti 3 Al and TiAl, showing the enhanced creep behavior of the intermetallics More
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Published: 01 January 2015
Fig. 3.26 Creep behavior of a number of terminal high-temperature titanium alloys and the intermetallic compounds Ti 3 Al and TiAl, showing the enhanced creep behavior of the intermetallics, particularly the equiatomic TiAl More
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Published: 01 January 2015
Fig. 6.33 Creep behavior of a number of terminal high-temperature titanium alloys and the intermetallic compounds Ti 3 Al and TiAl, showing the enhanced creep behavior of the intermetallics, particularly equiatomic TiAl More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080003
EISBN: 978-1-62708-304-1
... resistance alloys high-temperature corrosion IN MANY INDUSTRIAL SYSTEMS, plant operating conditions can be quite complex; it is rather difficult to use laboratory tests to simulate plant conditions. However, laboratory tests can provide good general guidance for making preliminary alloy selection...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2006
DOI: 10.31399/asm.tb.cw.t51820125
EISBN: 978-1-62708-339-3
...Abstract Abstract Nickel-base alloys used for low-temperature aqueous corrosion are commonly referred to as corrosion-resistant alloys (CRAs), and nickel alloys used for high-temperature applications are known as heat-resistant alloys, high-temperature alloys, or superalloys. The emphasis...
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Published: 01 March 2006
Fig. 3.19 Comparison of predicted and experimental axial fatigue results using the method of universal slopes equation and the four-point correlation method. (a) Low-alloy and high-strength steels. (b) Nonferrous metals. (c) Stainless steels and high-temperature alloys. Source: Ref 3.17 More
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Published: 01 December 1989
Fig. 4.47. Fatigue-crack-growth rates of long cracks for various high-temperature alloys in air at (left) room temperature and (right) 850 °C (1560 °F) ( Ref 186 ). More
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Published: 01 December 2000
Fig. 12.36 Scatter band for yield strength versus temperature of several cast titanium high-temperature alloys (Ti-6Al-2Sn-4Zr-2Mo, IMI 834, and Ti 1100) compared with cast Ti-6Al-4V More
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Published: 01 September 2005
Fig. 4 Influence of tempering temperature on core hardness of some high alloy steels More
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Published: 01 December 2004
Fig. D1.50 High-temperature aging characteristics for aluminum alloy 242.0-F, permanent mold More
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Published: 01 December 2004
Fig. D1.51 High-temperature aging characteristics for aluminum alloy 242.0-F, permanent mold. Specimens were aged for 2 years at room temperature prior to aging at these temperatures. More
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Published: 01 December 2004
Fig. D1.52 High-temperature aging characteristics for aluminum alloy 242.0-F, permanent mold More
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Published: 01 December 2004
Fig. D1.53 High-temperature aging characteristics for aluminum alloy 242.0-T4, permanent mold. Solution heat treatment: 6 h at 960 °F, quenched in 110 °F water More
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Published: 01 December 2004
Fig. D1.54 High-temperature aging characteristics for aluminum alloy 242.0-T4, permanent mold. Solution heat treatment: 6 h at 960 °F, quenched in 110 °F water More
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Published: 01 December 2004
Fig. D1.55 High-temperature aging characteristics for aluminum alloy 242.0-T4, permanent mold. Solution heat treatment: 6 h at 960 °F, quenched in 110 °F water More
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Published: 01 December 2004
Fig. D1.56 High-temperature aging characteristics for aluminum alloy 242.0-T4, sand cast. Cooled in still air More
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Published: 01 December 2004
Fig. D1.57 High-temperature aging characteristics for aluminum alloy 242.0-T4, sand cast. Cooled in still air More