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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...
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 of the casting alloy designation. The curves included are the results of measurements on individual lots considered representative of the respective alloys and tempers. The properties considered are yield strength, ultimate tensile strength, elongation, and Brinell hardness.
Book Chapter
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...
Abstract
In an attempt to explain the stresses encountered in the plastics industry, this article first defines the different types of internal stresses in amorphous polymers. Each type of thermal stress is then discussed in detail, with reference to the mechanism of generation and the effect 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 graphite fibers in amorphous polymers.
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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
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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
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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
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in Failure Analysis and Reliability of Optoelectronic Devices[1]
> Microelectronics Failure Analysis: Desk Reference
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] ).
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in Deformation, Strengthening, and Fracture of Ferritic Microstructures
> Steels: Processing, Structure, and Performance
Published: 01 January 2015
Fig. 11.12 Strain-aging effects on the yielding behavior of a low-carbon steel deformed to 4% true plastic strain and aged for various times at 60 °C (140 °F). Source: Ref 11.6
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Published: 01 January 2015
Fig. 16.3 Hardness of Fe-Ni-C alloy martensites at −195 °C (−320 °F) after aging for 3 h at the temperatures shown. Source: Ref 16.5
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Published: 01 August 1999
Fig. 4.19 (Part 1) Quench aging effects in ferrite. Rimming grade. 0.03C-0.005Si-0.43Mn (wt%). This series is continued in Fig. 4.20 . (a) Heated at 800 °C, cooled at 100 °C/h, solution treated at 700 °C for 1 h, water quenched. 105 HV. 1% nital. 250×. (b) Heated at 800 °C, cooled at 100
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Published: 01 August 1999
Fig. 4.20 (Part 1) Quench aging effects in ferrite. Rimming grade. 0.03C-0.005Si-0.43Mn (wt%). This is a continuation of the series shown in Fig. 4.19 . (a) Heated at 800 °C, cooled at 100 °C/h, solution treated at 700 °C for 1 h, water quenched, then aged at 50 °C for 2 days. 185 HV. 1
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Published: 01 August 1999
Fig. 4.20 (Part 2) (g) Variation in hardness with time at various aging temperatures; low-carbon steel water quenched from 700 °C.
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in Stress-Corrosion Cracking of High-Strength Steels (Yield Strengths Greater Than 1240 MPa)[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 3.30 Effect of aging temperature on crack growth rates in modified 18Ni-300 maraging steel. Source: Ref 3.8
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in Stress-Corrosion Cracking of High-Strength Steels (Yield Strengths Greater Than 1240 MPa)[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 3.31 Effect of aging temperature on K ISCC , K Ic , and yield strength of 18Ni-270 maraging steel. Source: Ref 3.8
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in Stress-Corrosion Cracking of Nickel-Base Alloys[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 5.40 Effect of stress intensity on CGR of alloy C-276 as a function of aging time at 500 °C (930 °F). Source: Ref 5.199
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in Environmentally Assisted Cracking of Uranium Alloys[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 12.6 Effect of aging temperature on times to failure of U-5Nb stressed to 275 MPa (40 ksi) in an aqueous solution containing 10 −4 N KCl. Source: Ref 12.15
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Published: 01 October 2011
Fig. 3.29 Natural aging curves for binary aluminum-copper alloys quenched in water at 100 °C (212 °F)
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Published: 01 October 2011
Fig. 14.15 (a) Phase diagram and (b) aging response of magnesium-aluminum alloy
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Published: 01 October 2011
Fig. 14.16 (a) Phase diagram and (b) aging response of magnesium-yttrium alloy
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Published: 01 October 2011
Fig. 14.17 (a) Phase diagram and (b) aging response of magnesium-zinc alloy
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