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Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140133
EISBN: 978-1-62708-335-5
... Abstract This data set presents aging response curves for a wide range of aluminum casting alloys. The aging response curves are of two types: room-temperature, or "natural," curves and artificial, or "high-temperature," curves. The curves in each group are presented in the numeric sequence...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2003
DOI: 10.31399/asm.tb.cfap.t69780295
EISBN: 978-1-62708-281-5
... on engineering properties. Methods of detecting and measuring internal stresses are also presented. The article then describes the combined effects of thermal stresses and orientation that result from processing conditions. Finally, it discusses numerous aspects of physical aging and the use of high-modulus...
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Published: 01 March 2006
Fig. 4 Schematic aging curve and microstructure. At a given aging temperature, the hardness of aluminum-copper alloys increases to a maximum, then drops off. Source: Ref 4 More
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Published: 01 December 2004
Fig. D1.28 Room-temperature aging characteristics for aluminum alloy 355.0-T4, aging time 120 days and less More
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Published: 01 December 1995
Fig. 22-8 The effects of “aging” and “aging plus carburization” at 982 °C (1800 °F) for 250 hours on the room-temperature ductility of cast heat-resistant alloys with 5 to 65% nickel and 19 and 25% chromium More
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Published: 01 November 2019
Fig 22 Plan view EBIC shows a top view of a stripe after aging. Defects originate at cleaving cracks at the bottom, and travel up and to the left. Once the defects cross the stripe, they quickly cause catastrophic failure. A drawing of this laser is also shown in figure 4 (after [4] ). More
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Published: 01 March 2002
Fig. 9.7 Aging curves showing hardness vs. time for selected nickel-base superalloys. Note the slow initial kinetics for IN-718. More
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Published: 01 March 2002
Fig. 12.11 Effect of solution heat treatment and aging on X-40 (HA-31) cobalt-base superalloy showing increase in strength resulting from carbide precipitation More
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Published: 01 March 2002
Fig. 12.13 Effect of aging on the rupture life and ductility of an as-cast modified Vitallium cobalt-base superalloy at 816 °C (1500 °F)/138 MPa (20 ksi) More
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Published: 01 June 2008
Fig. 20.10 Effect of aging temperature on 18Ni(250) maraging steel. Source: Ref 13 More
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Published: 01 June 2008
Fig. 27.6 Aging curves for Mg-9wt%Al alloy with various zinc additions. (Zinc compositions are given in wt%). More
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Published: 01 June 2008
Fig. 27.10 Effect of 205 °C (400 °F) aging on tensile properties of WE43A-T6. UTS, ultimate tensile strength; YS, yield strength. Courtesy of Magnesium Electron, Ltd . More
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Published: 01 December 2018
Fig. 3.35 Effect of aging time on strength and hardness in age hardening. Source: Ref 3.16 More
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Published: 01 October 2011
Fig. 14.15 (a) Phase diagram and (b) aging response of magnesium-aluminum alloy More
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Published: 01 October 2011
Fig. 14.16 (a) Phase diagram and (b) aging response of magnesium-yttrium alloy More
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Published: 01 October 2011
Fig. 14.17 (a) Phase diagram and (b) aging response of magnesium-zinc alloy More
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Published: 01 October 2011
Fig. 14.25 Schematic representation of the effects of aging. Source: Ref 14.10 More
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Published: 01 November 2010
Fig. 15.19 Compression strength versus aging time for PMR-15. Source: Ref 8 More
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Published: 01 November 2010
Fig. 15.20 Weight loss versus aging time for PMR-15 at 600 °F. Source: Ref 8 More
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Published: 01 August 2005
Fig. 2.9 Stress-strain curves for low-carbon steel showing strain aging. Region A , original material strained through yield point. Region B , immediately retested after reaching point X . Region C , reappearance and increase in yield point after aging at 150 °C (300 °F). Source: Ref 2.2 More