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Published: 01 January 1990
Fig. 11 CMSX-2 alloy development goal More
Series: ASM Handbook
Volume: 23A
Publisher: ASM International
Published: 12 September 2022
DOI: 10.31399/asm.hb.v23A.a0006907
EISBN: 978-1-62708-392-8
... of critical design parameters including chemical composition, flowability of powders, and melt surface tension. This article explains the fabrication methods of metal and novel alloy powders for medical applications. The development of zirconium alloy powder for laser-PBF is introduced as a case study...
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Published: 01 January 1996
Fig. 16 Fatigue crack development in alloy-depleted zones in 18% Ni maraging steel More
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Published: 01 December 2008
Fig. 3 Short sides of alloy 3 casting, showing poor development of surface layers More
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Published: 01 November 2010
Fig. 5 Development of macrosegregation in an alloy with interdendritic liquid lighter than nominal. (Lighter shade of     gray indicates liquid of higher-than-nominal composition; darker regions are depleted in solute. The white lines are the liquidus interface, the solid black lines More
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Published: 01 January 2005
Fig. 8 Micrograph of an IMI 829 alloy component processed to develop a fine, uniform, completely transformed beta microstructure More
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Published: 01 January 2005
Fig. 9 Micrograph of Beta-Cez alloy component processed to develop a controlled beta grain boundary microstructure to optimize strength and toughness. Courtesy of Timet More
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Published: 01 January 2006
Fig. 18 Dislocation substructure developed during simple shear of aluminum alloy 1050-O and 6022-T4 sheet samples (for different amounts of shear strain: ε 12 =0.5×γ). Source: Ref 177 More
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Published: 01 December 2004
Fig. 26 Microstructure of a cast aluminum-silicon alloy depicting well-developed dendritic structure. The dendrite arm spacing (DAS) is the mean center-to-center distance between the dendrite arms. More
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006722
EISBN: 978-1-62708-210-5
... Abstract Alloy 6156 is an Al-Si-Mg-Cu-Mn weldable alloy, developed for the lower portion of the fuselage, which required a T6 temper strength level and high damage tolerance properties. This datasheet provides information on key alloy metallurgy of this 6xxx series alloy. Fatigue crack growth...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006604
EISBN: 978-1-62708-210-5
... Abstract Alloy 2055 is an Al-Cu-Li alloy developed as a replacement for high-strength 7xxx and 2xxx alloys in applications such as fuselage stringers and floor beams. This datasheet provides information on its key alloy metallurgy and illustrates the damage tolerance of 2055-T84 extrusions...
Series: ASM Handbook
Volume: 24A
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.hb.v24A.a0006957
EISBN: 978-1-62708-439-0
... presents two key opportunities for AM related to automotive applications, specifically within the realm of metal laser powder-bed fusion: alloys and product designs capable of high throughput. The article also presents the general methodology of alloy development for automotive AM. It provides examples...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006711
EISBN: 978-1-62708-210-5
... Abstract Alloy 6013 is a high-strength Al-Mg-Si-Cu alloy, developed for extruded automotive bumpers. This datasheet provides information on key alloy metallurgy, processing effects on physical, tensile, static and fracture properties, and fabrication characteristics of this 6xxx series alloy...
Book Chapter

By A. Kearney, Elwin L. Rooy
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001061
EISBN: 978-1-62708-162-7
.... Alloys discussed include rotor alloys, commercial duralumin alloys, premium casting alloys, piston and elevated-temperature alloys, general-purpose alloys, magnesium alloys, aluminum-zinc-magnesium alloys, and bearing alloys. Six basic types of aluminum alloys developed for casting include aluminum...
Book Chapter

By B. Lynn Ferguson
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0003988
EISBN: 978-1-62708-185-6
..., alloy development, and inclusion assessment; and process considerations, such as process stages, tool design, and secondary operations; of ferrous alloy powder forging. The mechanical properties of powder forged materials are also reviewed. The article discusses the quality assurance tests for powder...
Book Chapter

By P.F. Tortorelli, S.J. Pawel
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003594
EISBN: 978-1-62708-182-5
.... It also provides guidelines for materials selection and alloy development based on liquid metal corrosion reactions. corrosion reactions liquid metal corrosion liquid metal environment liquid metal systems material selection CONCERN ABOUT CORROSION of solids exposed to liquid metal...
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Published: 15 December 2019
Fig. 45 Microstructure of as-polished Spangold (Au-19%Cu-5%Al), a jewelry alloy developed in South Africa, viewed in bright field (a) and Nomarski DIC (b). Martensite formation creates a rippled effect (“spangles”) on the surface. The specimen was hot-mounted, polished, and given the shape More
Book Chapter

By J.S. Robinson
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006262
EISBN: 978-1-62708-169-6
... Abstract Retrogression and reaging (RRA) is an established form of postquench aging heat treatment. RRA treatments can be applied to precipitation-hardened aluminum alloys that are used in aerospace applications. This article provides information on the development background of RRA...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006516
EISBN: 978-1-62708-210-5
... Abstract The development of aluminum alloys has progressed along two tracks: heat treatable and non-heat treatable. The Aluminum Association alloy composition limits and product temper are defined for major alloying elements. This article summarizes the historical evolution of the different...
Book Chapter

Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006609
EISBN: 978-1-62708-210-5
.... Alloy development included evaluation of various flow paths to reduce cost and enable efficient forming of the sections during the manufacture of the fuselage. Stretch forming of the T4 temper material was considered as a viable alternative. In 2010, alloy 2296 was registered by Constellium...